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17641.
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THE PROBLEM OF SPACE VEHICLE DESCENT IN PLANETARY ATMOSPHERES
by Ivanov, N. M | Martynov, A I. Description: vii, 45p.Publisher: Washington, D.C. NASA Availability: No items available
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17642.
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METHODS AND TECHNIQUES OF AIRFRAME STRENGTH FLIGHT TESTS
by Gudkov, A. I | Leshakov, P. S. Description: xii, 213p.Publisher: Washington, D.C. NASA 1973Availability: No items available
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17643.
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SALARIES
by Bokelman,Robert W.,Amico,D. A. Material type:  Book Description: 10.Publisher: Us Dept. Of Health,Education And Welfare, Washing 62-63Availability: No items available
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17644.
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METAL COMPLEXES-1 PREPARATION AND PHYSICAL PROPERTIES OF TRANSITION METAL COMPLEXES OF 6-MERCAPTOPURINE AND 4-MERCAPTO-6,7 DIPHENYL PTERIDINE
by Ghosh,K. A | Chatterjee,S. Material type: Book Publisher: Us Air Force Aerospace Research,, Bedford 1964Availability: No items available
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17645.
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AN EXPERIMENTAL INVESTIGATION OF THE SUBSONIC LONGITUDINAL CHARACTERISTICS OF FIVE SLENDER-WING MODELS WITH GOTHIC PLANFORMS.
by Kirkpatrick,D.L.I | Kirby,D A. Material type: Book Description: 46.Publisher: Her Majesty'S Stationery Office, London 1973Availability: No items available
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17646.
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MEASUREMENTS OF THE BOUNDARY LAYER AND WAKE OF TWO AEROFOIL SECTIONS AT HIGH REYNOLDS NUMBERS AND HIGH-SUBSONIC MACH NUMBERS.
by Cook,T A. Material type: Book Description: 89.Publisher: Her Majesty'S Stationery Office, London 1973Availability: No items available
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17647.
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THE ESTIMATION OF STRESSES AROUND UNREINFORCED HOLES IN INFINITE ELASTIC SHEETS.
by Sobey,A J. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available
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17648.
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OSCILLATORY-DERIVATIVE MEASUREMENTS ON STINGMOUNTED WING-TUNNEL MODELS
: METHOD OF TEST AND RESILTS FOR PITCH AND YAW ON A CAMBERED OGEE WING AT MACH NUMBERS UP TO 2.6
by Thompson,J S | Fail,R A. Material type: Book Description: 52.Publisher: Her Majesty'S Stationery Office, London 1964Availability: No items available
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17649.
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THE MANUFACTURE OF GLASS-BONDED FUELS FOR DOPPLER COFFICIENT MEASUREMENT.
by Ayer,J E,Hins,A G | Carpenter,D C. Material type: Book Description: 51.Publisher: Us Atomic Energy Commission,, Washington 1965Availability: No items available
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17650.
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SOME CHARACTERISTICS OF RECTANGULAR MULTI-SHOCK AND ISENTROPIC EXTERNAL COMPRESSION INTAKES AT A MACH NUMBER OF 2.9
by Dutton,R A | Goldsmith,E L. Material type: Book Description: 12.Publisher: Her Majesty'S Stationery Office, London 1963Availability: No items available
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17651.
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A FINITE-STEP METHOD FOR CALCULATION OF THEORETICAL LOAD DISTRIBUTIONS FOR ARBITRARY LIFTING-SURFACE ARRANGEMENTS AT SUBSONIC SPEEDS.
by Blackwell,James A. Material type: Book Description: 40.Publisher: Nasa, Washington, D.C. 1969Availability: No items available
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17652.
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GASEOUS-HYDROGEN REQUIREMENTS FOR THE DISCHARGE OF LIQUID HYDROGEN FROM A 1.52-METER-(5-FT-) DIAMETER SPHERICAL TANK
by Stochl,Robert J,Masters,Philip A | Dewitt,Richard L. Material type: Book Description: 62.Publisher: Nasa, Washington, D.C. 1969Availability: No items available
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17653.
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A METHOD FOR THE PREDICTION OF THE PROBABILITIES OF AIRCRAFT FATIGUE FAILURES WITHIN A FLEET OF KNOWN SIZE.
by Stagg,A M. Material type: Book Description: 30.Publisher: Her Majesty'S Stationery Office, London 1969Availability: No items available
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17654.
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ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF A NUCLEAR REACTOR SUPPORT STRUCTURE.
by Marchertas,A H,Fistedis,S H | Brittan,R O. Material type: Book Description: 100.Publisher: Us Atomic Energy Commission,, Washington 1965Availability: No items available
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17655.
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CATALOG OF NUCLEAR REACTOR CONSEPT.
by Teeter,Charles E,Lecky,James A | Martens,John H. Material type: Book Description: 161.Publisher: Us Atomic Energy Commission,, Washington 1964Availability: No items available
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17656.
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A COMPARISON BETWEEN TWO METHODS OF ANALYSIS OF OSCILLATORY PRESSURE MEASUREMENTS, ONE METHOD REQUIRING THE USE OF A TAPE RECORDER.
by Moore,A W | Welsh,B L. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office, London 1972Availability: No items available
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17657.
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EXPLORATORY TESTS ON A FORWARD-MOUNTED OVERWING ENGINE INSTALLATION.
by Kettle,D J,Kurn,A G | Bagley,J A. Material type: Book Description: 19.Publisher: Her Majesty'S Stationery Office, London 1972Availability: No items available
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17658.
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COMPARISION OF HELICOPTER AND AEROPLANE VERTICAL ACCELERATIONS IN TURBULENCE.
by Webber,D A. Material type: Book Description: 18.Publisher: Her Majesty'S Stationery Office, London 1966Availability: No items available
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17659.
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WIND-TUNNEL OBSERVATION OF BOUNDARY-LAYER TRANSITION ON A WING AT VARIOUS ANGLES OF SWEEPBACK.
by Anscombe,A | Illingworth,L N. Material type: Book Description: 9.Publisher: Her Majesty'S Stationery Office, London 1956Availability: No items available
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17660.
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MODEL TESTING TECHNIQUE EMPLOYED IN THE R.A.E. SEAPLANE TANK.
by Owen,T B,Kurn,A G | Smith,A G. Material type: Book Description: 59.Publisher: Her Majesty'S Stationery Office, London 1955Availability: No items available
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