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1. FUNDING REQUEST FOR THE CONCEPT FORMULATION PHASE OF AN ADVANCED AERODYNAMICS RECONNAISSANCE SYSTEM UNDER THE FY-69 GENERAL RESEARCH AND DEVELOPMENT (AIRCRAFT) BUDGET

   for the Concept Formulation Phase of an Advanced Aerodynamics Reconnaissance 25X1 System under the FY-69 General ... of a Aerodynamic Reconnaissance System. This is a new FY-69 effort and is appropriate to the General Research ... for the concept formulation phase of an Advanced Aerodynamic Reconnaissance System, under the General Research ...

2. FUNDING REQUEST FOR THE CONCEPT EVALUATION PHASE OF AN ADVANCED AERODYNAMICS RECONNAISSANCE SYSTEM UNDER THE FY-69 GENERAL RESEARCH AND DEVELOPMENT (AIRCRAFT) BUDGET

   Request for the Concept Evaluation Phase of an Advanced Aerodynamics Reconnaissance System under the FY-69 ... Aerodynamics Reconnaissance System under the FY-69 General Research and Development (Aircraft) Budget a) issue ... for the expenditure of to pursue the Concept Evaluation Phase of an Advanced Aerodynamic Reconnaissance System. ...

3. REPORT ON MEETING (SANITIZED) ON FEBRUARY 4, 1958,- INFORMAL DISCUSSION OF LTA AERODYNAMIC CONSIDERATIONS

   of LTA Aerodynamic Considerations The concepts proposed in Proposal 11510-B for powered plastic balloons ... ship. It was pointed out how the boundary layer concept of aerodynamics allows an Insight ... through the use of flow separation prevention techniques. To achieve these_aains, an aerodynamic research program ...

4. SCIENTIFIC ABSTRACT BABICHEV, V. Z.- BABICKY, A.

   Babichev, V.Z. TITLE: The Influence of Technological Factors on the Heat Loss and the Aerodynamic Resistance ... loss and the aerodynamic resistance are the basic factors determining the quality of an automo- bile ... Loss and the Aerodynamic Resistance of a Radiator and the same radiat-or for obtaining inore accurate ...

5. (SANITIZED)WORK ON MISSILES, 1936-1952

   Flow for the Production of a High Vacuum. VII. Use of Supersonic Diffusors in Aerodynamic Engines. ... The Problem: The Diffusor in Aerodynamic &gines. In all aerodynamic engines the following processes take ... A considerable limitation in the form of aerodynamic engines of all types is imposed not only by the fact ...

6. TASK ORDER NO. 2

   Electron.Mech. 9111.32 Nuclear Energy 9111.41 Ordnance 9111.51 34 200,0 Engr.Services 9111.61?fl Aerodynamics ... 9111.61 Aerodynamics 9111.71 Tool Engr. 9111.81 Pro.21!4 0 9111.91 /7 o Z /44 3 /o. Eng.Labor 9111 1-79 ... 911&912 /7 S44 131 271,00 i4. Eng. 0 H 9136 /qs / 733 111/ e r.Servicea 9111.1 p /049.4 Aerodynamics ...

7. SCIENTIFIC ABSTRACT ARZHAKOV, S.A.- ARZHANOV, Y.P.

   R. A~ Text Data Coverage: This is a textbook on theoretical aerodynamics. The first 1/12 I tin m I kn ... and aerodynamics of incompressible flulds, the second part Is dedicated to the aerodynamics of hIgher velocities ... Ch. I USSR- The Birthplace of Aerodynamics 5- 17 Development of hydro-and aerodynamics in the XVIITth ...

8. SCIENTIFIC ABSTRACT BESSONOV, A. F.- BESSONOV, A. P.

   possible aerodynamic resistance of the turning rotor in the gyroframe, etc. The proposed method ... of Aeronautical Instrument IMITTED: September 25, 1959 ard 212 FESSON A.-TY-1- A-G.------- Aerodynamic ... instruments) (Aerodynamics) 28(5) S/146/60/003/01/009/016 l(l) D002/DO06 AUTHOR: Bessonov A.G.j Candidate ...

9. FUNDING REQUEST FOR CONCEPT EVALUATION PHASE OF AN ADVANCED AERODYNAMICS RECONNAISSANCE SYSTEM UNDER THE FY69 GENERAL RESEARCH AND DEVELOPMENT (AIRCRAFT) BUDGET

   SUBJECT: Funding Request for the Concept Evaluation Phase of an Advancea,,Aerodynamic Reconnaissance System ... on the above subject. FY 1969 funding approval of II for a Concept Evaluation Phase of an Advanced Aerodynamic ...

10. CRUISE MISSILE DEFINITION (SALT TWO-663)

    WHICH SUSTAINS FLIGHT THROUGH USE OF AERODYNAMIC LIFT OVER MOST OF ITS RANGE," 2, THE FOLLOWING FACTORS ... IN THE DEFINITION, (8) "AERODYNAMIC LIFT" IS A KEY FACTOR IN DISTINGUISHING BETWEEN BALLISTIC AND CRUISE ...

11. PROBABLE AERODYNAMIC MISSILE FACILITIES KAPUSTIN YAR/VLADIMIROVKA MISSILE TEST CENTER USSR

    ('p~G DP02T06408R000900010030-8 JOINT PHOTOGRAPHIC INTELLIGENCE REPORT PROBABLE AERODYNAMIC MISSILE ... CIA-RDP02T06408R000900010030-8 JOINT PHOTOGRAPHIC INTELLIGENCE REPORT PROBABLE AERODYNAMIC MISSILE FACILITIES KAPUSTIN ... Aerodynamic Missile Facilities at the Ka- pustin Yar/Vladimirovka Missile Test Center. A similar analysis ...

12. SCIENTIFIC ABSTRACT MELNIKOV, A. K.- MELNIKOV, B. N.

    aerodynamic characteristics of wings of infinite span in supersonic flow, Influence of wing tips, lifting ... USSR/Aeronautics- aerodynamics Card 1/1 Pub. 135- 11/23 Author Mellnikov, A. F., Eng.-Col., Prof., Dr. of tech. sci. ... Eng.-Col., Prof., Dr. of tech. sci. Title High-speed aerodynamics Periodical Vest. vozd. flota, 4, 85-87, Ap ...

13. SCIENTIFIC ABSTRACT HOREJSI, J.- HORETZKY, T.

    himself In this volume to the analysis of aerodynamic forces and principles of propm1sion, Part II will deal with actual ... and tables. There are 36 references: 16 Czech, 2 Soviet., 11 German, and 7 English. Card 1/10 Aerodynamics ... Aerodynamics of Model Airplanes (Cont.) B. FUNDANENTAIS OF FLUID FLOW 2. Flow of Perfect Fluids 2.1. ...

14. FR:INZHENERNYY S. TO:INZH F.Z.

    *Aerodynamic contigurations. OPanele (Structural), Cylindrical bodies. *Flutter, Supersonic characteristics, ... and transverse bourocUng edgesu- oft of Tothmkw SWV*U (Mechanics--Aerodynamics, Tr, v. 9, no. 4) (over) ... 60, 62-18856 Nauk SSSR. Institut Mekbanivi vi~ ik n 960, Sborni r y DESCRIFrORS: *Aerodynamic ...

15. KAPUSTIN YAR CRUISE TEST COMPLEX D, SITE 1

    that have been associated with Complex D include probable large surface-launched aerodynamic missiles,' the DR-1 ... aerodynamic missile program. Most of the permanent structures had been completed by September 1957. ... probably used by another large, surface-launched aerodynamic mis- sile. Other additions to Site 1 included ...

16. MEASUREMENTS, AT MACH NUMBERS UP TO 2.8, OF THE LONGITUDINAL CHARACTERISTICS OF ONE PLANE AND THREE CAMBERED SLENDER OGEE WINGS

    Variation of aerodynamic-centre position with lift coefficient, M 0.3 24. Variation of aerodynamic ... speeds. The present tests contribute to an extensive investigation of the aerodynamics of slender shap(s ... the centre of lift at cruising condition-. near the position of the aerodynamic centre at low speeds), ...

17. FUNDING REQUEST FOR THE CONCEPT EVALUATION PHASE OF AN ADVANCED AERODYNAMICS RECONNAISSANCE SYSTEM UNDER THE FY-69 GENERAL RESEARCH AND DEVELOPMENT (AIRCRAFT) BUDGET

    Comptroller, OSA SUBJECT: Funding Request for the Concept Evaluati)n Phase of an Advanced Aerodynamics ... Comptroller, OSA SUBJECT Funding Request for the Concept Evaluation Phase of an Advanced Aerodynamics ... for the expenditure, of to pursue the Concept Evaluation Phase of an Advanced Aerodynamic Reconnaissance System. ...

18. MILITARY SCIENCE PROGRAM AT THE POLYTECHNIC INSTITUTE IN BUCHAREST

    chemistry students went into the chemical warfare phase. oq Aerodynamics students were assigned to the air ... semester, five other aerodynamics students petitioned the school military authorities for an assign- ment ... to the air force phase on the basis that they were studying aerodynamics. This petition was granted ...

19. TASK ORDER NO. 2

    Aerodynamics 9111 71. Tool En r 9111 81 g.. Pro Su v 9111 91... Eng Labor 9111 f G G 3 y c. r r c / ce ... j O Aerodynamics 9111.71 Tool Engr. 9111.81 Pro. Su v. 9111.91 ~i o i!~, r yv Eng.Labor J Z c Y 4 3! ... Nuclear Energy 9111.41- Ordnance 9111.51 7/ O Bagr.Services 93-11.61 /4 ', / Z ' Aerodynamics ...

20. POTENTIAL SOVIET REACTIONS TO A US STEALTH FIGHTER

    with the purpose of lowering electronic paramagnetic resonance (EPR) and developing aerodynamic forms ... the enemy air defense zone at low altitude; at medium and high altitudes they will be, from an aerodynamic ... having the usual aerodynamic design, because the aircraft weight is distributed along the entire wingspan. ...

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