SCIENTIFIC ABSTRACT WIRTH, Z. - WISLICKI, T.

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December 31, 1967
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SCIENTIFIC ABSTRACT
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UIRTH, ZDLNEK, ed. I liatiborice; statni zarek a babiccino udoll. (,Ua-,rni stat napsal Zde,-2ek Wirth. -'polupracovali: Gohumll Novak, et al. 'VYd- 3, v STI 1. V Fraze, Statni telovychoviie nakl., 1955?) 28 p. (Ratiborlce; the state castle and Grandinother(Is Valley. 3d ed. illus., maps) SO: Monthly Index of East European Accossibns (EEAI) LC, Vol. 7, no. 5, &,* 1958 WIRTH ZDENEK "Sychrov, statni zamek a okoli. (Titulovou stat napsal Zidenek Wirth. Spolupraco Bohmmir Lifka at al. 2. rozirene vyd. V Praze, Sportovni a turisticke nakl., 1957) P. 32 (Publikace Statni pamatkove spravy) (Sychrov, the dtate castle and its surroundings; a tourist guide. 2d enl. ad. illus.., nap plans) P. 32 (Praha, Czechoslovakia) Monthly Index of East European Accessions (EFAI) LC, Vol. 7, No. 7, aly 1958 BROZKOVA, V.; WIRMOVA, Ii.; KUBAT, A., MUDr.; SYEIIIRA, J. Our experience -wdth radioactive iodine ir. the diagnGsis af thyropathies. Plzen. lek. sborn. 24:83-88 164 I. Klinlka chorob vnitmich lekarske fakulty University Kar- lovy v Plzni (prednosta: prof. WDr. K. Bobek) a onkologicke oddeleni SFN v Plzni (zast. prednosta: MUDr. Al.ois Kubat). I WISCII1U. H.J Dipl. Ing.; KULDA, V., inz. [translator) Excitation of synchronous machines by rectifiers. El tech Gbl-:,r 5,3' no.10:529-532 0 164. 1. VEB Elektroprojekt, Berlin, German Democratic Republic (for Wischer). WISGICKI, Marok _T&Anological progress in welding. Wiad elektrotechn 31 no.12'. 293-296 D'63- 1. Zaklad Vytworezy AparatmT.'- :ii~idzielon6j A~!M& -Waromma. WISILEWSKI -SWATEK) Stanislaw --Llxdwik Anodic decomposition of graphitized electrodes duringelectrol~sis. Ft-.2. Sodium chlorate. Chemia stooow 5 ro.2t299-310 161. 1. Katedra Elektrochemii Technicznej i Elektrometalurgii, Politechnika Slaska, Gliwice i Instytut Chemii Nieorganicznej, Gliwice. SZR3WNR, Wald~rslaw; DZARNDCKI, Wilhelm; WISKOVf-BUCZKOVSK4,jWina, JANICKI,Andreej ft% Studies on liver-protecting substances. I. Observations on experi- mental poisoning with carbon tetrachloride.. Pat.polska 6 no.l: 1-6 Jan-Mar '55. 1. Z Zakladu Patologli 0golnej A.M. w Gdauskm -Ueravnik: prof. dr, W. Szreder I z Zakladi Anatomli Patol. A.M. w Gdansku. Kierownik prof. Dr. W. C%arnocki. Adres: GkIansk. Zaklad Patologii Ogolnej i Doswiadcsalnej, Debinki 7. (CARBON TMRACHIORIDIC, poisoning, exper.) (POISONING, experimental. carbon tetrachloride) wIsKONT-BUGZKOWSU'Ah~' exchange in hypoxic-hyp-ercaPuic hypothermia in rats. Acta physiol. polow. 8 no-3:50-568 1957. 1. Z Z~kjadu yizjologii A 9 w Gdanaka. Kierownik: prof. dr B. Szabuniewicz. (RISPIATION, Physiolous eff. of bypothermias hypoxic-hypercapnic in rat (Pol)) (HYPO BXMIA. effects, on gas exchange in rat, hypoxie-hypireapnic technic (Fol)) W'i -"na, 76 m rg L. da Of Z n~-- c - L dQ.: J Oj a F;:6 4 rio - il- Ag 63, 16 Z ~FrQOU F 1 ZJ Oll Og 1 J. P-k6(Nmi.1 :14eJyczrAej wMar Au 7 1 e rown'l~ wi cz). prof dr. Szabunia WISKONT-BUCZKOWSKA, Halina 1-1- --- -- - .. Histamine metabolism in pregnancy and gestational activity of progesterone. G-inek. Pol. 35 no.32439-"8 14y-Je 164 Histamine In human labor and pregnancy. lbid.2449-456 1. Z II Kliniki Poloznict,,ra i Chorob Kobiecych Akademii Medycznej w Gdansku (KierownikI., prof. dr. med. R.Gromadzki). PAPIFIROUSKI, ~'bignisw Comparison of results of 1=.jrologic pregnancy test no.4-423-427 Ar, 165- Pichheim-7cndeck test. Gi.neks Pole 36 1. Z II KIJ.niki Polomict-wa i Chorob Kobiecych AIIA w Gd4rw;kLj (aerownik: Prof. dr. med. We Gronadzki). peal ratows beefilk" wo lius. The 11"M tally, Isably %ihofoiaft ~- I'll ~ C~Anmfgcwllmi Wily locim- lie , viry S the Gerumns- Ivy I-Pin Stefisn, mgr Inz.; URBANlKI, (Ir %he position of Analysis cf modern r~&.thcd3 of -L 4 -1 gec-d 35 361 no. 32 a Ohip at sea. Pt- 2- 1'rza, 9P,-Iol Mr 164. WISLA, Stefan mgr inz. Terminology in the field of maritime hydrography and its tasks. Friegl good-34 no.10:422-425 0 '62- ..WISIA,.,Ste mgr. inz.; 7irbanskij, Jozef, dr- Analysis of modern methods of determining the position of a ship at sea. Przegl. geod. 36 no.2t57-.60 F164 -...L-4,1032-66. 13C ACC NRt AP6 SOURCE CODE% PO/0082/66/000/002/00, AUTHOR: WIslaq S. (Mader engineer.' Lieutenant) ORG: none TITLE: A simplified method of determining the accuracy of a ship's P081#1on plot, SOURCE: Przeglad moreld, no. 2,, 1966, 64-73 &6~ TOPIC TAGS: phip navigation celestial navigation, navigation aid ABSTRACT: Analyzed are evaluations of average error M in ship's position plots calculated from two or three reference lines. The author presents several tables and a nomogram assist-, Ing In rapid determination of M for calculations with two or three reference lines derived from: sightings, radiolocation, distance, or height of celestial bodies. The technique of using the 1 cited tables and chart Is Illustrated by several practical examples. Calculation time Is about J! 1 min and the results insure adequate accuracy of the plot. Orig. art. has: I figm, 3 tables, and 7 formulas. SUB CODE: 17/ SUBM DATE: none/ ORIG REF: 004 IfEBSKIp Marian; WISLAWSKA, Barbara A case of parathyroid adenoma with..signs of Recklinghausen's disease and severe anemia. Fol. tyg. lek. 17 no.5:182-184 29 Ja-162. 1. Z II Kliniki Chorob, Wewnetrznych AM w Lodzi; kierowrdk: prof. dr med. Jerzy Jakobowski. I (OSTEITIS FIBROSA compl) (ANEMIA HYPOCHROMIC etiol) IZDEBSKI, Marian; WISLA14SKA Barbara-__ Acute allegic toxic syndrome fo3-lowing meprobamate (miltOW09 P4DI- tyg. lek. 17 no .10:363-364 5 Mr '62, 1. Z II Kliniki Chorob Wewnetrznych AM w Lodzi, kierownik: prof. dr nauk med. Jerzy Jakabowski. (MEPROBAKATE toxicol) (ALLERGY) g g=,,g:!jj)g 'g vg F: WW MINOR OWN Hill I'l IN I, I WISLAWSKI, Jerzy, WOLTM, Halina Temporal arteritis. Neur. &c.polska 5 no-3:27?-285 My-Je 155. 1. Z Kliniki Neumbirurgii A.M. w Wareumle. lierownik: -prof. dr J. Chorobaki. i z Kliniki Okulietyczuej A.M. w Warssawie. Kierou-nik: prof. dr W.H. Nelanovski. (ARTMTIS temporal, clin. aspects) KOZNIEWSKA, H.; WISLAWSKI,J; SLOWIK,T. Epidermoid cyst of the spinal cord. Neur. &c polska 10 no.2:213-217 mr-Ap 6o. 1 Z Kliniki Neurochirurgii A.M. w Warszawie Kierownik: prof. dr med. J:Chorobski. (SPINAL CORD neopl) KEPSKI, Apolinary; WISLAWSKI, Jer2y Case of total blocking of Magendie's foramen in an adult. Nseurol. neurochir. psychiat. pol. 12 no.6:925~-928 162. la Z Kliniki Nourochirurgii.AM w Warazawic Kierownik: prof. dr J. Chorobski. (ITEUROLOGY) Clinic -Uto 'IT'd ep. .1i -e &demiii tied r S !I'! pi'lontdalis)." F coree, ' 4:1 c t I~ft,2; pp 11579=1611. 10 7 male and I fw4 1e Clinicp ,I datp on I r., p 'th, sual suraica tvc&ted by tbe u t5 oF whom v e. 6 V q4k'~S ~1, Jerzy; MAZUROWSKI, Witold; LEWICKI, Zdzislaw Metastatic tumors of the brain. Nowo-twory 14 no.3,253-257 Ag-S 164. 1. Z Kliniki Neurochirurgii Akademii Medycznej w Warazawle (Kierownik; prof. dr. med. L. Stepien) i z Zakladu Anatomli Patologicznej Akademii Medycznej w Warszawie (Kierownikt .doc. dr. med. R. Stanczykowa). WISLAMSKI,_,~erzy,;, JTIAFTEK, Jan; ZARSMI, Stefan Co-existing 2 cerebral tLunors originating from different embryoniL- formations. Pol. tyg. lek. 19 no.30:1165-1166 Z7 J1164 1 1. Z.Kliniki Neurochirurgii Akademii Medycznaj w Varnawie; kierownik: prof. dr. med. Ijicjan Stepieno JISL9491 M "Interesting ideas on resin collectiezell p. 24 (Jas nojakj~ Vol. 26, No. 2, Feb. 1952, Warszawa) East European Vol. 3, No. 3 SO,s MoAh LiBt of Accessionsi/Library of Congreasp March 1951., Uncl. WMIAWSKIS M. WISIAW9KI., M. Sinplified method resinifying spruce* p9 Be Vol. 29, no. 10, Oct. 1955 IAS.,POLSKI AGRICULTUM mcchAn PP- 314-319, 2 fjR,,. LWJ"" Pl~;914d BudowIsny. No. ?__S. "lepixing the definition, M"h&nfZlktlon of worof b"', "Ifthankation Index And .Ingle Ournparally, . k. XXIIIAnAtion. on Of [tie ba'SIC me nalyals 't both Indices And the b4al, of exit -X of Indkv. In pla,lell"'llizatiln In 'he cOmequent a gripir" IhOdf by Meallm ning. An pygM dox AS one of the MAI doption nf th rimmi. to n find fundamuqtAl lplnnt r 111('11antitalln Interlink Ill. pj4nllbjjt 14tes 141141 "I'llimmne indkrx . d tie Caro-Ing fill( 77he doterni, it by Mralul nf tj* t viring In building A More throuch na,,'n * this link CCU of M" PrActke in Analyalm of the, features ft- 'hanization ronjuell. wilth the proXce" "Itic Of bulc Mach 1,,rDetertnination of th Agnitude In the IWO. Y,. 0 in w the required for ;he mechanlf-f* "Unit .he fun- Immo L 62t.96/ lish Teohnical Abstracts P 9 r planned Per-IndIc Preventive- Overhatils rl teni 0 S o 1953 No 4 rs . Th ;NVIJII At 'd 11Y ns , Advance 1 1jamy Plant, According, to sugXesti t . , d , ra Con r~l On Con ' : C Building Industry an the 10, in "t6w elq~ . eh z3poblegawczych rPmN l Architecture nOwY "SY4:.:= Pla~:)%va-term h W!dtug PrOJelctu 1OX31%. prieglAd Suda Mjs,yn bulawlinyc ' kich - 31r__318.4 tabs. &' 195,~ p~. 0. wiany. N be carried out, In a*system of P12r'-,t,.i eco lant should RapILM to p The sYAtem Ad0D't!d In Pa- ce,)rd3nee with a datalled Plan. l i I n a nomyt A sys'wn Of Plknne~l p-2r-j eve-Itive overhaul- ~ i3nnezi pr land relle3 On p .o. cl6sely the Ir'tPrvCnI.1g ked out 4.0 define tic overh3uls ha3 been ooliod bitween such Polish Technical Abstracts 4t 1953 No Foudallo"S for the PRIMOU of c(Illurt an,l sclell,e, Building Industry and Oudowi fund,,,,,-nt6,, I I Pr7,cglld Dii. dowtany. Na, 10. 1932, Pp- 30-38j, 11 figs. Arohitecture 0foundations for the highest pirt of the Palac3 of Culture and Science form a 7-metre high reinforoed co'ncrete box rcughly -to n, ua area. The foun:Wlon Plate *Of' tile re!nforccj X 70 r co 0:1-a, concre*.e I)-L5C. MOre than lo cantl co:I,Crptc L-,JX L~ L"'d 'mn iram--dLa'ely on the bottom ld of 4he exca re! verUcal baulaga of ma. VaLlon. Horl erlais was effectei~-:?--- --mi-O,Fhc--vY cranes hO's I L.:V ~6. Vie reInforcament was carried out in the forn, .( gr,ds Aad la 1, 5 moasurlag~-.P-to 66 -,q- The shutteriig f,-~r ti, was -Iff-- fgrm 2 Mrnerele the w7 r e~ d ovej again. of large P'ates and angles, capable of %cing v U~ed Ov r an 3056 93A5:7nM j, Production of Large Prefabricaied Cellfec Slabs at the J. %tallm Memorial Palace of Culture and Science.. ,,Produkcja wielkich ptefabrykowanych plyt gtropowych mi bu- dowle Palact- Kultury t Nsuki Im. J. Staltna". PriRglqd Budowlany. No. 8, 14 , ", pp. " M4)-26 1, 4 figs., I tab. Prefabricated slabs ar- being used in conistruction of cetlings not d-igned for h-rizontal sUffening. The slabs are made In special mnutd-%. nctually, on the building site. As a rule, steam curing of the stab$ takes 23 hours, which I.-; adequate to produce a strength of R = 0,75 Rf~4. Given proDer production organigatlart, correct design of th,- glabs and 01.- 1- ~f ".-, -.:-t- f .-h 1IMPIC WISLICKI, A. (INZYNIERIA I BUDOWNICTWO, Bol. 10, No. 11, Nov. 1953, Warszawa, Poland) "The industrialization of work on the building site of the Stalin Place of Culture ard Science in Warsaw,* P. 330 SO: MONTHLY LIST OF EAST EUROPEAN ACCESSIONS, L.C., Vol. 3. No. 4, APRIL 1954 WISLICKI,A. ItConcrete Work On The Bu4 Min - Site --Of The- Palace Of- Culture And Science" P. 11. (Przeglad M Vol, 25, no, l.-Jan& 1953, Warszawa) East European Vol- 3. No.2, SO: Month List of 1=32= AccessionsY /Library of Congress, Februar7, 1954 1993:, Uncl. I&TSLICKT; A. ure And ssembling The Steel Frame.of-The Palace Of Cult ~y rszawa) WISLIC j p,. I yOVIAWZYK) - R. "A 1953, Wa =L . -Vol. 25,, no. 3j. Mar Science :[n Warsaw" p. 67- (Prze lad-BudOulany Fast Europpan Vol* 3j No., 2; as, FebruarY., 1954 "U.,.Uncl- a= Accessionsi/LibrarY of COngre so'. tMth List Of/Xu rf "-e C,~,'rl -.-rlks ";flz;cll cn, the ;,-rial cent-cros; cc aL tho Pala zawa, Pollard) jql,~, Wars 0.12, Dec* 1101 3, so: KontblY List of East Phuro-11-C-M-1 C~,Cces:3io-,S, 1954, Uncl. ' T JISLici-I, A. 110-reanIzati(,n in lbuilding 7,rilaf--r -f, Warsaw" (,-ID-`]GIdUl fit,ki AIN, Vol. ib. 10, Cdolvr 3.954, 'larsaw, Poland) SO: - Yonthly List cT East Furopean Accessions (TT--,AL)j I,C~ Vc!, 4, 10. 3; Mareh 1955, Uncl. WISLICKI, A. "Winter work on the conetruction of the 1. Stalin Palace of Ciilture and Science In Waraqw." P. 377. (PUZErIGLAD BUDOWLM. Vol. 26, No. 12, Dec. 1954 Warozawa, Poland) SO: Monthly List of Bast B"dpean Accessions. (EFAL). Lo. Vol. 4, No. 4. April 1955. Uncl. WISLICKI, A. "Horizontal, Trarmport in the Construction of the Hi_,7hesf- Parts of 4.r:-- Stalin Palace of Science and Culture in Warsaw#" P.54. (PRZWLAD MRIMNY Vol. 75, No. 2, Feb. 1954. Warszawa, Poland) 30; Month3,y List of East European Accessions, (EEAL), LC, Vol. 4, No. 1, Jan. 1955 Unel. WISLICKI, A. Influence of the Palace of Culture and Science on technical progress in Polish building. p. 110. Vol. 12, no. 4, Apr. 1955. IN M IRRIA I BLUMUCTWO. Warszawa. Source: East European Accessions List (EEAL), IC, Vol. 5., no. 3., March 1956. 300-December 7, vol. 2, Feb. 19515, Monthly UA !)f -I U', Vol. 4, "'X-Y art j,,Uj-ot(,,ajj pcce,~isir-in.5, 195~,, Uncl. The Greeks were not only great architects but also building managers, P. 82. (PRZEGLAD BUDOWLANY, Warszawa, Vol. 27, no. 3., Mar. 1955-) SOt 'Monthly List of East European Accessions., (EEAL), LC, Vol. h, No. '61 4~ 1955, Uncl. TWISLICKI, A. Pumping mortar. p. 121. Vol 27, no. 4,- Apr. 1955. PRZE-GIAD BUDOWU'T'I. Warsaw, Poland. So: Eastern European Accession. Vol 5, no. 4, April-1956 ItrISLICKI,_A. The opening of Stalin's Palace of Culture and Sciences in Warsaw. p. 233 PRZEGLAD BUDMILANY Warsz&wE- Vol. 27, no. 7, July 1955 SOURCE: Ealit European Accessions List (ERAL), LC, Vol,/5, no. 3, March 1956 WISLICKT, A. Development of mechanized h1lildin.q and its- iniustrializa,lion P. 32. Vol. 4, no. 1, Jan. 1956 POZEIIIII STAVBY Praha, Czechoslovakia Source: Last European Accession List. Librery of Conigm-ass Vol. 5, I-To. 8, August 1956 WISLICKIP A. WISLICKI, A. Trends in the development of rechanizatIon and the production of buildinp raebinerr. p. 29 Vol. 5, no. 10, Oct. 1956 BUDOWNICTWO FRIZEFS1 (Y;,~E FOI ITICAL SCIENCE , Warsiawa, Poland. So: East Eurorean accession Vol. 6, No. 3, March 1957 WISLICKIp A. WIS-LICK-Iq A. Mechanizing the building industry. p. 128 Vol. 28P no.3, Mar. 1956 ..PRZEGLAD BUDaiLM TECHNOL40GY Warazavap Poland So: East European A ccession,, Vol. 6. no. 2. 1957 WISLICK11 A. WISLICKI, A. More attention to historic remnants of technique. p. 198. Vol. 77, no. 5, MaY 1956 PRZEGLAD TECHNICZNY PHILOSOPHY & RELIGION Warszawa, Poland SO! East European Accession, Vol. 6, March 1957 WISLICKI, A. "Today and tomorrow of the Museum of Technology of the Central Technical Organization." P. 101 (Przeglad Techniczny) Vol. 70., no. 3, Feb. 1958 Warsaw, Poland SO: Monthly Index of East European Accessions (EEAI) LG. Vol. 7, no, 4, April 1958 WISLIC KI, A TECHNOLCGY Periodicals: PRZEGLAD BUD%MANY'f Vol. 30Y no. 7, July 1958 WISLICI~T-, A.. Comparison of the mechanization of the construction industry in the USSIR, the United States, the German Federal RepublIc., and Poland. p.261. Monthly List of East European Accessions (IYAI) IC, Vol. 8, Fo. 2,,, February 1959, Unclass. WISLICK-T. Alfred, doc. inz. Mechanization of finishing works. PrzegI budcrr-11 i Imd --iasmk. 23 no.80-13-514 Ag'61. HIM WISLICKI, Alfred (Warszawa) Testing thd usefulness of new types of building machines. Prhegl budowl i bud mieszk 33 no.7413-415 JI 161 WISLICKI, Alfred (Warszawa) Dynmnics of the development of building m-echamizatirn. P--Zegl budowl 34 no.3:151-159 Mr 162. 1. Czlonek Kamitetii Redakcyjnego miesiecznika "Przeglad Budo-vilany." WISLICKI: Alfred, doe., -Marlp inz. (Warsaw) Dynamice of thO devolopmnt of builAing industr7 mchanization* : I*ohanizace noo9:108-12.1 162.' Ins stavby 10 no.9:Suppl WISLICKI, Alfred., doc., inz. (Varsava); TOTH, Ladislav, inz. (translator] Efficiency of building machilras and their manufacture in various countries. Inz stavby 10 no.UsSuppl.04dchanizaca no.lltl3l-134 162. 1. SNR, Bratislava (for Toth). X WISLICKI, Alfred (Warszawa) ~-~~~Once Fg~the need of educating mechanical engineers for 1 the building industry. FrzegI Vudowl i bud Mie3ZLC 34 n0-9:473-- 474 Ag 162. DZWONKCWSKI,'Kazimierz (Warszawa); KOZIITSKI, Wieslaw (Warszawa); WISLICKI qf;m~=aiW - - Mechanization of finishing works. Przegl budowl i bud mieszk 34 no-9:544-548 S 162* W WISLICJU -,-Altreds doe* inze, Methods of determining the usefulaeoo of construction machiner7. Przegl budowl i bud mieszk 35 no.lt65-68 Ja f63o WISLICKI,'Al~red; MOLIVSKI, Roman The state of equipment supply at constructior works in Warsaw and ways to improva tho situation, Przagl budowl i bud mieszk 35 no,9; 483-485 163. 0 0 WISLICKI. Alfred,._doc. inz. Operational testing of the aptitude of earthwork machines in Poland. Inz stavby 12 no. 2: Supplement: Mechanizace. no. 2: 17-20 164. 1. Ustav organ12ace a mechanizace stavebnictvi, Varsava. BRACH, Ignacy; ROjEK, Karol; yjpjjqKj,_,.Alfred (Warszawa) International Conferenci'on Mchoknization in Earth-dor1k. Przegl budowl i bud mieszk 36 no.3:1506~1-51 14* '64- WISLICKI, Bogdan On the possibilities of increasing the combustion heat of hydrocarbon fuels. Przam chem 39 no.51240-244 MY 160. Ir P1101 204~7 D227/D305 04P/005/001/002 AUTHOR: TITLE: Increasing the heat of combustion of hydrocarbon fuels PERIODICAL: PrzemysR: chemiczny, v. 40, no. 5, 1961, 240-244 TEXT: This is a discussion on the possibilities of improving jet ai-rcraft fuels by adjusting the hydrocarbon combustion and by us- ing B, Be, Mg, Al or their derivatives. Heat given out by a fuel can be increased by incorporating components possessing high heats of combustion. This is the fundamental criterion of fuel quality, depending only on the-ililtial mixture and..products of combusti-on. Complete,oxidation of C and H gives: I KgC + Kgo Ll Kg CO + 8140 Kcal 2 2 1 KgH + 8 Kgo 9 Kg H 0(steam) + 28800 Kcal. (2) 2 2 2 Card 1/19 20437 -P/014/61/040/005/001/002 Increasing the heat of D227/D305 From the percentage amounts of carbon (c) and hydrogen (h) in a particular compound, the heat given out in combustion is given by: Qd = 81.4 C + 288 h Kcal/Yg = 'lower' calorific value (3) and Ag = 81.4 c + 341 h Kcal/Kg = heat of combustion ('upper' calorific value). (4) For jet and turbine engines, combustion heat is the most important fuel property, since this determines the exhaust velocity of air and, hence, the thrust. For compounds containing oxygen, Eqs. (3) and (4) become: 0 Qd = 81.4 c + 288 (h Kcal/Kg (5) Qg = 81.4 c + 341, (hl- Kcal/Kg. (6) Jet fuels are chiefly derived from distillation and d-wzical treat- ment of petroleum and coalta~. In the USA 1.39 5.6 and 18 million Card 2/19 20107 P/014/617d4O/OO5/001/002 Increasing the heat of ... D227/D305 tons were produced in 1950, 1954 and 1958 respectively and produc- tion is expected to reach 30 million tons in 1964. (Ref. 3: Reak- tivnoye toplivo USA, Moskva, 1956); (Ref. 4: Petroleum Proc., 10, 343v 1955); (Ref. 5: World Petrol, 28, no. 11, 55, 1957); and according to E. Bass, J. Lubbock, C. Williams (Ref. 8: Proceedings of the Third World Petroleum Congress, section VII, Leiden). Total heat evolved in burning is the sum of the individual heats of com- bustion, 40 % of the energy being due to H and 60 % to C which constitutes 84 % of the fuel by weight. Calorific values of various hydrocarbons containing equal amounts of C are shown in Table 1, while those for a number of homologous hydrocarbon series of inter- est are contained in Table 2. CCalorific values of hydrocarbons may be discussed in terms of the . ratio which forthe fuels in question varies from 5.7 to 6.7 with corresponding Qd values of 1-0,000 109500 Kcals/Kg, and in connection with the boiling points, since these determine which compounds will be associated in a given fraction during manufacture (Figs. 2 and 3). The value of (Q g_Qd) Card 3/19 2C437 P/014/61/040/005/001/002 Increasing the heat of ... D227/D305 is 770-800 Kcals/Kg for alkanes, 750-770 for alicyclics and olefins and r\j38O for benzene homologues. Calorific values and H-content of alkanes fall with increasing b.p. For single-ring alicyclics Qd is little affected by the b.p. and it increases in higher homo- logues of the benzene series due to the H-rich side-chains. NaDh- thalene homologues have lower calorific values than benzene, eg. n-Bu benzene 99459 Bu-naphthalene 9P535 Kcal/Kg. The calorific va- lue per liter Q, (= Qd - x density) is more sensitive to chemical composition than Qd (Table 3). A few examples are quoted showing that Q, of alkanes, cycloalkanes and alkenes changes appreciably with the structure of the carbon skeleton. For the aromatics Qg de- creases and Q1 increases on addition of an aromatic ring with a 1-2 carbon side-chain. The thermal efficiency of fuels can, there- fore, be increased by including compounds of high Qg and densityg bearing in mind the composition and b.p. considerations. Thus the Card 4/19 F,101 204 7 4/61Y~40/005/001/002 Increasing the heat of ... D227/ '305 calorific value of jet fuels (lo,250-10,350 Kcal/Kg) may be raised to 10,400-10,500 Kcal/Kg by using a parafin/olefin mixture of den- sity ~-iO.77. Raising this value to 10,500-10,600 with fuel densi- ty > 0.77 is considerably more difficult. Fuel usefulness also de- pends on the melting point, viscosity, corrosion characteristics, vapor pressure, inflammability, rate of combustion, frame stabili- ty, coking tendency, engine design etc. ZIbstractor's note: These factors are not discussed7. The calorific values for a number of fuels are given in Table-4. Certain metals and non-metals and their compounds are otentially useful fuels because of their high heats of dombustion Uable 5). The usefulness of these elements is assessed by means of a "fuel index" X, defined by X Qvol' (7) 0 0 Kt , Qvol where Qwt and Qvol are the calorific values of the material tested, 0 per Yg and per liter respectively, and Q S are the corresponding Card 5/19 20437 P/014/61/040/00r-1/001/002 increasing the heat of D227/D305 values,for paraffin oil 0 0 109280 - 89540 = 87.8 - 10 6 Kt 0 Qvol = Values of X for certain materials of interest are listed in Fig. 4. Use of hydrogen which possesses the highest heat of combustion is deterred by its unfavorable physical properties. In the search for better fuels (1): Be and B can be usefully substituted for C in a hydrocarbon molecule or, alternatively, (2): Suspensions or colloi- dal solutions of metallic powders in hydrocarbons could be employed (1): Interest in B and its compounds has grown recently, although its.physico/chemical properties have not as yet been fully investi- gated. Boron hydrides with calorific values > 15,000 Kcal/Kg are of particular interest. Certain properties of these and related compounds are shown in Tables 6 and 7. (2): Suspensions are pre- ferable to colloidal solutions, where the achievment of high con- centrations presents serious difficulties. Life of the suspensions may be prolonged by increasing the hydrocarbon-viscosity and by stirring, Physical characteristics of A120 3 p B203 , BeO, Li2o' 14go should also be considered since they may absorb considerable heat Card 6/19 20437 11040100510011002 P/O 14/ i.ncreasing the heat of D227/D305 in melting or even vaporizing, and being solids, will accelerate both.erosion and corrosion of engine parts. Recent American work on boron and its derivatives for us6 as aircraft and rocket fuel is briefl mentioned. The author considers that at present -the use of Al(BI-1 Li and 3 hydrides.allows a.50 0 increatie in engine 4 3 thrust. As an illustration, the maximum flying distances of a 58 ton plane with 125 m3 tanks are quoted as 16,000-35,000 kin for the above mentioned metals, hydrides and metal suspensions as opposed to 14,500-15,000 kin of the conventional fue Is (15,000 for kerosene). There are 4 figures, 8 tables and 28 references: 11 Soviet bloc and 17 non-Soviet-bloc. References to the four most recent English- language publications read as follows: H. Harvey, World Petrol, 26, no. 10, 54, 1957; H. Harvey, SAE. J. VIII, 65, no.9, 17, 1957; I.R. Cracknell, Plight, 71, no. 2512, 332, 1957; Ind. Eng. Chem., .49, 1265t 1957. Card 7/19 P101 2 37 4/6 1%4 0/005/001/002 !. ~Increasing the heat of ... D227/D305 Table 1. Oompoeition and value ST,blla,l, Wartodd O~;Io'W'**Orsx Wad Slementarny rdinych of various hydrocarbons. 'rAtLF Igrup wqg1owodordwd) egend: 1 Hydrocarbon; 2 qslowod6r 2 6r SkIAd eleme~tarny Wartold GO Palowa kcal/kG - formula; 3 - composition; H, -1. C. -I. TI t01.. J 'Og6rna 4 - calori fic value, kcal/kg; Ufeksn ql~' I q g 1: 83.74 M98 11560 5 - lower; 6 - upper; 7 - he- k... . Zne , , ~"': a 1 ~ 85.72 20615 '1". xane; 8 -h exene; 9 cyclohe- k1oheknn QUIS 11 C 14,28 7 60 83'n 92 31 10379 9533 11150 16H0 xane; 10 benzene. 0 4 , , Table 1. Card.8/19 20437 111014Z61100100510011002 j -icreasing the heat of ... D227/D305 Table 2. Distribution of the calorific value in homologous series. rmAr 2- T a b I I c a 2. Hoskind Warto1c) OPRJOW#j W Arzeregach homologfrx- Series; 2 - lower Legend: 1 VC111PT), calorific value (kcal/Kg); Wortold ot)Alown dolnA kcal/kO n-alkanes; 4 - iso-alkanes; Smell homoloalmy 5 R-olefins; 6 - -s-117gle-ring C. alic7yelice; 7 - double-ring ali- No-41a Paraliny ID is"s 10570 10540 1f"3 cyclics; 8 benzene and homo- frop4rallay 40 Normalne ole(Iny 0 1"15 IZ33 10163 30513 10470 Mll 101,64 logous; 9 naphthalene homolo- 0 kl 11M 16"s IWO gous; 10 - aromatic-cyclopara- o ey Dwilplericleillowt ffin hydrocarbons., Q0 Dowell I jtgo hams. 5393 "AS "17 - ITOM010KI nattalenu(i) - 9"1 105 - WQitlO%VO(lGTY Table 2. t yet iie-eyk lops rA fl.j ltUW# Card 9/19 20437 Increa the heat of in P/014/61/0 D227 D305 40/005/001/002 s g / Table 3. 'Calorific values per : T a b I i ca3WartodA opalowe z kRograrns I z 11tra iwi4xk6w +'kg and per liter for various priedstawisjqcych Poswre961ne szeregi hoinalogtezried) 1 416LE compounds representing parti- 0 ~3) ';"We cular homologous series. Wqgtowod6r W~lr d.- I keel/kC ~fj kcalil Legend: 1 - Hydrocarbon; (D n-Efekan. 0 De C.H. C H 8,7bg 0 7ft IN70 18183 7080 7740 20 cen-2 . W l , 2 - formula; 3 - density (d Butyloeyk1ohekson O Cjr- 9.7M lam am 4 4 - calorifid values; (BDekaUna (trans) CwHp 6.872 10165 rM 5 - kcal/Y 6 kcal A GDekaHna (cis) -I)But (1 lob C.U1, 11 q 0,890 0 3 10225 9M 9100 M g; 7 - n-decane; 8 decene-2; - enzen y C.,retraiins, . 1. I.C~.H.' ,VA S.Sq3t V23 9450 .9 - butyl cyclohexane; Gmetylonaftatien q.H. 1.025 92*4 961-5 GNafta lotnicza (11rc) IMSO 8300 10 - trans-decalin; 11 - cis- decalln ; 12 - butyl'benzene-, 13 - te tralin; 14 - methyl naph- thalene; 15 kerosene. A .J Card 10/19- increasing the heat of ... Table. 4. Calorific values of fuels and the constituent hydro- carbon groups. Legend: 1 - Fuel; 2 density, 15-0/15.50; 3 - boiling point, OC; 4 - group composition, %; 5 - calorific value; 6 - aroma- ties; 7 - cycloparaffins; 8 alkanes; 9 kcal/Kg; 10 kcal/1; 11 aviation fuel; 12 kerosene; 13 - alkane con- centrate; 14 - alkane/alicyclics concentrate; 15 - aromatics con- centrate; 16 - aviation spirit; 17 - diesel fuel. 4 ; . ; Card 11/19 P/01 416 ?W4'9/005/001/002 a b I i*~~ "WahM Cl'opafowe Pal1w I Frup woglowodordw weho- dzqcych iw Qclad Pallwa) (D " . T a Sklad grupowy 1A. Warto9k ~opalowa Pallwo D W. Aro- Maps- Ik' Ll I licit M Rty- raft. rall- CInO r1owe kG I nowe Aliwo lotnt- Yeze 01765i 60-270 - - - 10150 TOO ,N&fta lotnicu 0,7910 155-"0 19.4 39.2 41,4 IOUG 8135 ~C..cent,.t )-,jwqglowodo- r6w parall- nowych 0,7475 159-265 2.6 3.2 97.2 10,10 "23 ?ComentrAt I wqK10wodo- JA r6w parafl- '-' nowych I c7- klopjlraflno- ~! Wych 0,7010 100 -274 1,4 51,9 40,7 10100 1133 Koncentrat e~,WqKlowodo- r6w aroma- lycznych O,e545 156-253 75.2 11.4 13,4 SS60 -0 n yna lot- " 1C .1 CZ3 0,7103 50-1" 1 faltwo do all- nik6w diesia Q.tIOG -1 10058 8?20 Increasing the heat of ... Table 5. Heats of oombustion -ce tain of r substances. legend: 1 - Aluminum; 2 - pe- trol; 3 - beryllium; 4 - magne- sium; 5 - -hydrogen; 6 - silicon; 7 - acetylene; 8 - titanium; 9 - lithium; 40 - lithium hydride; 11 - carbon; 12 kerosene (pa- raffin oil); 13 boron; 14 tetrahydro diborane, B2H6; 15 borane, B2H6; 16 - pentaborane, B5119; 17 - decaborane BjoH14; 18 - suspension of B in kerosene 19 - suspension of B in pentabo- rane; 20 - AL 140 atm.absolute (above 1 atm) and 1 OOC; 21 - AL 350C; 22 - AL 9900; 23 - aub- stance; 24 heat of combustion; Card.12/19 20h-37- P/014/61/040/005/001/002 D2 27/D305 03 Clew 59412MI& W, w iq Sto Un k fl Substanell d 12'r OM . charak haty ftbity rystymny kcal/l (d1s nat- (dia nat- ty - 1) ty - 1) Mn 28043 2,U 7400 0.12 1.71 3enzyna 7280 0.85 104" 1.01 a." cry' 29950 3.31 111" 1.57 5,40 agnez 10300 1.21 P, 5933 0.51 0,70 Yod6r al 9- 0,04 2we 2,70 1.05 c,--- i7ece 2," 7330 0.71 1.47 tcetylen 7150 0." 11520 1.12 0.2 1 ryton :0520 2.40 4350 0,44 , 1.0 ~,t 5170 :, : 10265 1 3,00 2.63 Nodorek litu 8060 3 : 9050 0.93 a," 11520 2,01 1830 0.75 1,59 qatta IS40 1,00 10290 1.00 1.00 Br 32100 3,76 1"30 1,34 5,17 "w"O"w"dr , 132114 T705 Oil 17436 1.10 1.57 picrohydrobo- rowod6r 82110 93W0 1.10 19700 1,11 1.78 riqc1oborawo- ' d6r BsHe 9876 1.13 16110 1.58 1.83 resiqclobor- C~5 1 wod6r BlaH14 13250000) &,85 14400 1,40 1 1 1.91 ~awlestna boru w nafele 20500 3.40 12"G 1.25 3.10 wlestna boru a ~ w BSHq 21350 2.50 14400 1.40 ' 20437 P/014/61/040/005/0011/002 Increasing the heat of ... D227/D305 1e 5. (cont'd) Tab 25 - kcals per liter; 26 - relative to paraffin oil (paraffin oil - 1); 27 kcals per kg; 28 relative to paraffin oil (paraffin oil 1); 29 - fuel index. Table 6. Characteristics of some boron hydrides. legend: 1 Compound; 2 - formula; 3 melting point (0C); 4 boiling point (0C); 5 spec. gravity; 6 - vapor pressure; 7 gen. properties; 8 - stable pentaborane; 9 decaborane; 10 - borazole; 11 - aluminum borohydride; .12 - beryllium borohydride; 13 - lithitn borohydride; 14 - not decomposed in air between 0-100C. Slowly hy- drolyzed by water; 15 - does not ignite or decompose, slowly hydro- lyzed; 16 - chemically stable, soluble in water? not hydrolyzed in the cold; 17 violent reaction with air and water; 18 - violent reaction with air and water; 19 stable in moist oxygen. Card 13/19 Increasing the heat of Table 6. (cont'd) T a b I I c to 0. Churn ktorystyka n1ektdrych borowallar dw 0. to- 11. 107, 1. r. Q Temp.C) -remp. Zwlqtck 6r wrz. ,c Plqctoborowod6r trwaly (15,1 przy II DzieACcloboro- 99,5 I 213 wod6r (156 przy 162 B.N.U. 130row0doro- Horowodorek jillnu Al Uorowodnrek be. Be rylu Borowodorek litu L--i7i- Card 14:/19 2007 P/01 4/61/040/005/001/002 D227/D305 CD Clqtar Pr4tt m Winsnold og61ne Nlnieiwy per 0,610 Gatio.) nle, rozklada siq na pu-- mm) W) awletexu w 0 do 10'. "1 dzialantem H--O ulega Do- wolnemu rozkladowt 0.92 1 19 (low) We Zoppla Sig* nie Illega mm) (99 ) r.zktndwA . ulga Onwol- nel hydroUxle 53 0,8519 chemiante trwaly. ruzpla- szczalny w H-0 bez roz- kladu. nrzy ogrzanlu hy- - - drolizuJe - (Bit.). -6314 .44,3 0,3508 1 FS (I-) 9waltownle rengule z HzO (t3. I Dowletriefp (DIIJ, 31 91p jak WYtej 237 0,668 trwaly w atmosferze tle- P nu I wilgod 20437 11/014/61/040/oor.-,/ool/002 ncreasing the heat of ... D227/D305 Table 7. Heats of combustion of boronand beryllium derivatives. point (OC) Legend: 1 -. I-lame; 2 - formula; 3 density; 4 - melting 5 - boilin point (00); 6 - lower calorific value; 7 -o- kcalAg; i 8 -.kcal/N 9 - boron; 10 - beryllium; 11 - pentaborane; 12 - de- caborane, 13 - aluminum borohydride;.14 - beryllium borohydride; 15 - lithium borohydride; 16 - dimethyl beryllium; 17 trimethyl boron; 18 - triethyl boron; 19 - tripropyl boron; 20 trimethyl aluminum; 21 tetramethyl diboroethane.. Card 15/19 V Increasing the heat of ... Table 7. Tablica 7-Clept o spalanta zwlqzk6w boru I berylul) J Nazwa 61. Bor 13cryt Be PIPdoborowod6r B'11. gVzlesjqc1oborowod6r 131.111. O)Horowodorek glinu At (1311A O)lJormodorek berylu Be (BU.). CsAwowocsarek -litu LfUlf, OiDwumctyloberyi Be (CHA CRT/rralmetylobor 13 (Cit.). (f- Tr6jetylobor P B (C.14% Qj'frr6jpropylobor D AM). (Rerr6imetyloglin A] (Cl 1.), gCxterometylodwubora- C 1 1. CH. etan, , /D \ CH. C11, Card-16/19 p"A" Tern p 0., to Te, (P mina wartole-opalowa p C -C (5) kCaljkG 1 0, kcalti 2,3 l Btu y 13670 31400' 1,01 Ma ,y 15000 2100 0,61 -m-45,% Be 15340 9630 0.92 99 - 15310 14tol 0,356. '-65,4 44.5 1=0 17670 31 $1.3 16100 - 0.666 273 roiklade siq 14300 9500. - Staly 17700 (11900) 0.42 -20 11900 0,59 to-" 11200 0.72 - ISO - ""0 0,73 15 125 10550 11500 2o437 P/014/61/040/005/001/002 D227/D305 20437 P/014/~1/040/005/001/002 increasing the heat of ... D227/D305 Pig. 2., Relationship between the calorific value and the,Iratio. (D Legend: 1 - Upper calorific tyfLOPAROWK value (kcalAg); 2 -.2 ratio; I I IN MMO &I papuNry I'. P-11 H , 3 - aromatics; 4 - alicyclics; 5 - alkanes; 6 - petroleum pro- -A ducts. 5 to it f2 t3 9 Is J 7 0 Fig. 2. ST04UNIM C:t4 20437 P/014/61/040/005/001/002 Increasing the heat of ... D227/D305 Fig. 3. Dependence of the cal,orific.value on boiling point. Ito legend: 1 Lower calorific value (kcalAg); 2 - boiling point, 00; 3 - alkanes; 4 alicyclics; 5 - aromatics; 6 - double-ring hydrocarbons -bstractor's note: Not clear ZA whether aromatic or alicyclig. loom Fig. 3. 1 Card 18/19 Do WC610WOOORY PAROINOWr _OX 8 X 1647 OW 149 WO jzU ZDU 0 TEMPIRA TURA WRIENIA, *C Increasing the heat, of Fig. 4. Fuel indices of various substances. legend: 1 - Beryllium; 2 - bo- ron; 3 pentaborane; 4 - alu- minum; 5 - carbon; 6 - diborane; .7 - silicon; 6 - titanium; 9 - paraffin oil (kerosene);. 10 - acetylene; 11 - lithium hydride; 12 - gasolene; 13 - magnesium; 14 lithium; 15 - fuel index. P/01 ygol')J40/005/001/002 D227 "305 0, 1 UYNAIN IMAUXURKWUNY (OwsA nys. 4. Wspd1citynniki charaktoryA me OIA neragu substancjl w Fig. 4. Card 19/1Q 266:13 P/008/61/ooo/oo8/002/003 /A 0/00 D235/D302 AUTHOR: Wislicki, Bogdan, Master of Engineering TITLE: Dependence of the completeness of,combustion of turbine and jet engine fuels of chemical consti- tution PERIODICAL: Technika lotnicza, no. 8, 1961, 171 - 178 TEXT: The effects of chemical constitution of hydrocarbon fuels on the combustion efficiency and tendency towards coking were investigated. Chemical characteristics of jet and turbine fuels are specially important when they affect the physical properties. Heat evolved in combustion is lower than the theoretical amount, since a certain amount is wasted in side reactions such as pyro- lysis or the formation of carbon (coking and smoking). Thermal efficiency, , is defined as the ratio of the heat actually obtained tor6e lower calorific value of the fuel. Complete- ness of combustion is given byO, (=~z x 100), and may reach Card 115 Dependence of the... 26613 P/008/61/000/008/002/003 D235/D302 94 _ 98% although 75 - 80% is more usual. The combustion process is based fundamentally on turbulent mixing and molecular dif- fusion of air and fuel vapor. Stability of the flame and the rate of combustibn strongly affect Z; Thus rapid oxidation at 18oo - 20000C with a nearly thporetical amount of air should yield continuous combustion. The mixing process at these tem- peratures is considerably slower than the rate of combustion. Combustion of cyclohexane in -varying amounts of air is quoted as an illustration. Oxidation of hydrocarbons proceeds by a chain mechanism, w-ithout branching, and is accelerated by the products of pyrolysis, of which hydrogen is especially important owing to its rapid ditfusion. Effects of the structural char- acteristics of the fuel are discussed. Fuels of higher molec- ular weight are less efficient due to their tendency towards cracking. Self-ignition is more likely in the case of paraffins than with aromatics and ignition is, therefore, more delayed in the case of the latter. Pre-ignition processes have not been fully investigated, but unfavorable re.actions at that stage may Card 2/5 26613 P/008/61/000/008/002/003 Dependence of the... D235/D302 lower the thermal efficiency. Laboratory measurements of 0 have been carried out, under high altitude conditions, for aviation spirit (boiling range 53 - 1740c). Effects of the air/fuel ratios on 0 have been investigated for kerosene, paraffin concentrate 6f'boiling range 159 - 2650C and a mixture of aromatic (75.2%) cyclopaSaffins (11.4%) and paraffins (13.4%) boiling between 1~6 and 253 C. Values are given to show that the optimum air/fuel ratio is -, 60, corresponding to a 0 of 98% for all the fuels considered. The aromatic fuels became considerably less effic- ient with high proportions of air. Design of the combustion chamber in relation to 0 is briefly mentioned, quoting Western sources, and experimental values of 0 are given for hydrocarbons fed into the experimental chamber by injection or evaporation. The effects of the chemical nature of the fuel on 0 appears to be more Pronounced-in the latter case, 0 decreasing in the order: paraffins > single ring cycloparaffins >cyclo-olefins > double ring cycloparaffins > single ring aromatics with a side-chain single ring aromatics ~> double ring aromatics. Proportions of Card 3/5 26613 P/008/61/000/008/002/003 Dependence of the.-.-. D235/D302 the constituents and the boiling range also have an effect. In- complete combustion results in smoking and deposition of coke or in the elimination of soot and carbon particles in the exhaust gases. They physical nature of smoke is briefly described, showing that smoke is easily eliminated before coagulation into soot. Dehydrogenation of the fuel and polymerization of the carbon skeletons leads to coking. The effects of coke deposition on various parts of the engine are shortly described. Coking tendency is ultimately related to the design of the combustion chamber, degree of atomization, surface tension, viscosity and composition of the fuel and the amount and pressure of air. Coking increases with increased fuel density, b.p., and in the order: paraffins 4, cyclo-olefins < aromatics. These relation- ships areillustrated. Within each group, coking increases with decreased yolatility and in general increases for the higher C ratios. Smoke formatfon increases in the series n-paraffins< Yf iso-paraffins /_ cycloparaffins < olefins /-, cyclo-olefins < Card 4/ 5' 26613 P/008/61/000/008/002/003 Dependence of the..... D235/D302, di-olefin alkynes ~ n-alkyl benzenes. This is discussed andil- lustrated. Sulphur Tompounds increase coking, but not as mucy as the aromatics, which however do not exceed 25% in the usual fuels. The tendency towards the inclusion of a hi5her percent- age of less volatile components into the American P5 and JP6 fuels is mentioned. Improvement of combustion efficiency may partially alleviate this, problem, especially during the pre- ighition and i nitioj3 stages. W6stern work in this field is shortly descrited.' It is believed that suitable kerosene ~~els githout any adeitives can be PrQduced. There are 19 figures tables and 2 references: 5 Soviet-bloc and 19 non-Soviel- .bloc. The references to the four-most recent English-language publications read as follows:' J Sharp, J. Royal Aeronautical Ljoc. 58 no 528, 813~ (1954)- V:F. Massa-and B.B. Russel U.S. Pat. 23~19,.10491, March 20 195L E.C. Aughes and 0. Hook Petr6l 71 107 ( Eng., no .19~6); and I.B. Hinkamp and V. H1nzd Ind. Eng. Chem., 47, no. 8, 1560.~(1955)- Card 515 WISLICKIP Bogdan, mgr. C, . I Combustion accuracy of fuel for turbine and rar--Jet engines and its chemical composition. Techn lotn 16 no.8;171-178 Ag 161. 7 1 ACCESSION NR: AP3008291 P/0008/63/000/009/0233/0242 AUTHOR' Wislicki, Bogdan TITLE: Some pro~lem;`~`offtl kinetics of chemical. processei in the combustion chambers ofaircraft turbine engines SOURCE: Technika lotniczal n6. 9, 1963, 233-242 TOPIC TAGS: kineticaq aircraft turbine combustion chamber- heat transfer,. aerodynamicshydrodynimic; ignition, mass transfer The-author defines his pa'er as "a g6neral introduction to'the kinetics ABSTRACT: p ''I er of th~ processes of the combustion of hydrocarb6n P und the combustion conditions In turbine engines," remarking that there has thu's far been in Poland no exhaustive study of this subject from the viewpoint of 'thi'kinetics of chemical reactions at high speeds and around,2000C. Sinclelthe tate~of*combustlon and its Intensification are.limited by the processes ofq~ heat and transfer, only a pg its kineti ..,.total conception of the problem. gained by obsery'i' cs,-ae~rodynamics and hydrodynamics can explain a number of phenomena and establish their regularity. Card 1/2 ACCESSION NR: AP3008291 There are sections entitled: "Chemical kinetics of combustion reactions' I'Mechanism of chaiii~self-lgnltlonil! "Machani*sm thermal self-ignition,11 and "Kinetics of chemical reactions in the f I ame. 11 Original aPticle has !19 figures and 44 numbered formulas. ASSOCIATION: SITK, Warsaw SUBMITTED:. 00 DATE ACQ: 1406t'63 E~ i ICL -00 SUB CODE: AC, NO REFISOV:, .00711 OTHER: 001 1z Big Card 2/2, T MIELVIKOWA, Boleslawa, doc. inz.; WISLICKI, Bogdan, mgr.1 KLFINp64aniBJ mgr* Evaluation of fuels for turbojet engines. Inst lotn prace no.18t 19-33 163. 31 WISLICKI, Bogdan, mgr Combustion procemses of hydrocartxmi fupls in fli;-I'd firjw ongIncs. Techn lotn 19 no.6.14~-149 Je 164. Specific heat valu-s of certaln hydrocprty)n fuelti. lbl.d.~~2 of cover, 3-4 of cover atjTfd 4 W Pr-4 VOTMrNB, _401,TO,97 'Ap P72532/64~~W/023/00~2!003~, I~M- ORt Wisli ki B. (Vislitskiy, 3,) (Master of arts); K jKzUzhanovskUy., R.7~v taster engineerl 1TITLEi Mini for fuel testing SOURCEt Warsav. Instytut Lotnictwa. Prace, no. 23, 1964, 22-35 ',TOPIC TAGSt combustion chamber, fuel test, continuous combustion, vibration combus-, !tion ABSTRACT: J, Wolfa rf thz! Polish n1S2+ji+,j!Le has designed a small-size 1-an- bustion cham ft,-Ft n a fuel conbustioiA investigation in order to Oefine as the chaxacteristics -f combustion =ih ev~aporWlon under conditions compar-nWe to -real engine operatIng conditions. The chamber, designed for visual observa-__-)n .of the combustion process, has been used for comparative study of B-70 gasoline and P-2 fuel at fuel fl-w rates from 0.2 to 1.5 kg/hr. The chamber's thermal efficiency as a function of air "xoess for the above fuels was determined. The testB conducted have demonstruted tiir~ usefulness of microchambers for the investigation of fuel -7cm- bustion with evaporatkon.. It has also been shown that by the use of diffusion i-f* _k/2 L C .~.FA PDrs it is Possible to intensify the vib-ati le- fue.1 ya onal combustion-. A detailel scriptiOn of the combustion chamber and test stand is presented, Orig. art. has: )j formulas and 24 figu-res. [AC] ASSOCIATIONt Instytut Latnietwa, Warsaw (Aeronautici3 Institute)-ly SUBMITED r COMp-r64 KIM: CID SLM CODE. F-p REF SOV, 007- ATD PRzss.- 3220 OTHER. 9 0--)(_1)2b-67 F,.-,TP(t)/ETI IJP(c) JD/WB ACC NR: - '_ * I AT6033638 SOURCE CODE, PO/2532/GG/000/026/0042/0061 AUTHOR: I~Ijslicki, Bogdan -- Vislitskiy, B. (Master of Arts) ORG: Institute of Aviation, -Warsaw (Instytut Lotnietwa) TITLE: High efficiency laboratory fractionating column SOURCE: Warsaw. InstyAut Lotnictwa. Prace, no. 26, 1966, 42-61 TOPIC TAGS: fractional distillation, petroleum fuel, fuel oil, resistance thcri-nometer, petroleum refining, laboratory fractionating column, petroleum fraction, electronic dephlegmation timer, temperature control/MET-42 temperature control unit A13STRACT: The author discusses an automatic, laboratory- type, packed fractionating column for distilling petroleum fuel oils and petroleum fractions unde normal or reduced pressure, which he had designed, built, and tested. Maximum column efficiency is about 140 theoretical plates with 1. 7-cm plate equivalent spacing, retardation is 0. 71 milliliter liquid per plate, and a pressure drop of 0. 142 mn-i 1-1.0 per plate. The column can also be used on pilot plant scale for fractional distillation of liquids which do not corrode the packing material. Senior _A~ C.,d 1 2 UDC: 66.048:665.52 L 09026-6? AT6033638 Technician Zdzislaw Kaminski of the Fuels Laboratory, Institute of Aviation, Warsaw cncllaborate~) in constructing the column. The "L" packing material was chosen, and the electronic timer for automatic dephlegmation control was planned and built by Dr. A. Maczynski. Institute of Physj~;al C4~jMjqtEy,_?A1 A~ay~saw. The 'MET-42 differential temperature control unit and the precision resistance thermom eter, wf;,-re built at Departm ant C of Physics, Warsaw Poj)~echniSL Institute accordincy to the design by J. Czernik, Master of Engineering. The paper was approved by Dr. Andrzej Maczynski, Master of Arts. Orig. art. has: 32 figures, 12 tables, and 8 formulas. [Based on-author's abstract] SU13 CODE: 11, 21/ SUBM DATE: 00Jun65j ORIG REF: 003/ SOV REF: 006/ OTH REF: 006/ ABGAR(YdICZ, Franciszek, prof. dr; BURZYNSKI, Bohdan; WISLINSKA, Irena; WITCZAK, Franciszek Fattening of young cattle using aDMOniated dry sugar-beet pulp with a differing content of nitrogen compounds in the rations. Zesz probI post nauk roln no.41:101-106 163. .-I. Katedra Zywienia Zwierzat, Szkola Glowna Gospodarstwa Wiejskiego, Warszawa. Kierownik: prof. F. Abgarowicz. WISLINSKI, M.; STUDZINSKI, T. Hematological studies on types of hemoglobin in sheeD. Acta physiol.polon. ll,no-5/6:916-917 160. 1. Z Katedry Fisjololgii Zwierxat Wydzialu Weterynaryjnego W.S.R. v Lublinie. Kierovnik: prof.dr. W.Holobut. (HEMOGLaBIN) POLAR/Chemical Technology. Chemical Products and T~heir Application Synthetic Polymers. Plastics Abs Jour: Ref Zhur-Khim., No 13, 1958, 45111. Author Wisliski Tadeusz. Inst Title Bonding of Non-Metals. Part 11. Technology of Bonding. Part III. Bonding Flaws and Pundamentals of Bonding Control. Orig Pub: Techn. lotnicza, 1956, 11, No 4, 1o6-116; No 6, 167-173- Abstract: H. A review. The technology of preparation of ad- hesives and of their application to non-metallic surfaces are considered. Detailed description of clamping procedures, heating during bond formation, and methods for shortening the periocl of setting. Card V2 POLAND/Chemical Technology. Chemical Products and Their Application. Synthetic Polymers. Plastics Abs Jour: Ref Zhur-Khim , No 13, 1958, 45111 III. Consideration of flaws arising at the surfaces being bonded, and of their causes; fundamentals of quality control of bonded articles and of determina- tion of the characteristics of adhesives. Card 2/2 H 51 I-JISLICFT, T. Metal gluing. Pt. 2. (To be contd.) P. 146 (Technika,Lotnicza. Vol. 12, no. 5, Sept./Oct. 1957. Warszawa, Poland) Monthly Index of East Liirope~n Accessions (ER.Al) LC. Vol. 7, no. 2, February 1958