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1958 NASA/USAF SPACE PRIBES (ABLE-1)

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BookPublisher: Nasa, Washington, D.C. 1959Description: VIII,84.DDC classification: NASA | MEMO 5-25-59 -

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA MEMO 5-25-59 - (Browse shelf)	Not for loan		TR7957

Total holds: 0

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Previous	NASA MEMO 5-20-59L LOW-SUBSONIC MEASUREMENTS OF THE STATIC AND OSCILATORY LATERAL STABILITY DERIVATIVES OF A SWEPTBACK-WING AIRPLANE CONFIGURATION AT ANGLES OF ATTACK FROM-10 D/C TO 90 D/C	NASA MEMO 5-23-59L WATER-LANDING CHARACTERISTICS OF A REENTRY CAPSULE	NASA MEMO 5-24-59L A SIMPLE METHOD FOR DETERMINING HEAT TRANSFER, SKIN FRICTION, AND BOUNDARY-LAYER THICKNESS FOR HYPERSONIC LAMINAR BOUNDARY-LAYER FLOWS IN A PRESSURE GRADIENT	NASA MEMO 5-25-59 - 1958 NASA/USAF SPACE PRIBES (ABLE-1)	NASA MEMO 5-25-59L INVESTIGATION OF THE STABILITY OF VERY FLAT SPIN AND ANALYSIS OF EFFECTS OF APPLYING VARIOUS MOMENTS UTILIZING THE THREE MOMENT EQUATIONS OF MOTION	NASA MEMO 5-26-59L MODIFIED MATRIX METHOD FOR CALCULATING STEADY-STATE SPAN LODING ON FLEXIBLE WINGS IN SUBSONIC FLIGHT	NASA MEMO 5-28-59L INVESTIGATION ON THE USE OF A FREELY ROTATING ROTOR AT THE COWL FACE OF A SUPERSONIC CONICAL INLET TO REDUCE INLET FLOW DISTORTION	Next

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