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LOWP-SPEED WIND-TUNNEL STUDIES RELATING TO PITCH-UP ON A SUPERSONIC TRANSPORT MODEL WITH A HIGH-ASPECT-RATIO VARIABLE-SWEEP WING

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BookPublisher: Nasa, Washington, D.C. 1966Description: 73.DDC classification: NASA | TN D-3542

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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 TN D-3542 (Browse shelf)	Not for loan		TR17707

Total holds: 0

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Previous	NASA TN D-3528 GOLD REDUCTION AS A MEANS OF REDUCING EMBRITTLEMENT OF A COBALT-BASE ALLOY (L-605)	NASA TN D-3529 DISTRIBUTED PARAMETER ANALYSIS OF PRESSURE AND FLOW DISTURBANCES IN ROCKET PROPELLANT FEED SYSTEMS	NASA TN D-3530 FIBER-METAL COMPOSITE MATERIALS	NASA TN D-3542 LOWP-SPEED WIND-TUNNEL STUDIES RELATING TO PITCH-UP ON A SUPERSONIC TRANSPORT MODEL WITH A HIGH-ASPECT-RATIO VARIABLE-SWEEP WING	NASA TN D-3543 THERMAL DISTORTIONS OF THIN-WALLED PARABOLOIDAL SHELLS	NASA TN D-3544 STATIC STABILITY CHARACTERISTICS OF CONE AND HALF-CONE-PYRAMID CONFIGURATIONS AT MACH 6.83	NASA TN D-3545 PRESSURE MEASUREMENTS ON RIGID MODEL OF BALLUTE DECELERATOR AT MACH NUMBERS FROM 0.56 TO 1.96	Next

Bound With Nasa Tn D-3541,3543-49

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