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THE EFFECT OF PROTUBERANCES, CAVITIES, AND ANGLE OF ATTACK ON THE WIND-TUNNEL PRESSURE AND HEAT-TRANSFER DISTRIBUTION FOR THE APOLLO COMMAND MODULE

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BookPublisher: Nasa, Washington, D.C. 1966Description: 57.DDC classification: NASA | TM X-1243

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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 TM X-1243 (Browse shelf)	Not for loan		TR16207

Total holds: 0

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Previous	NASA TM X-1214 TRANSONIC AERODYNAMIC CHARACTERISTICS OF A TAILLESS FIXED-WING SUPERSONIC TRANSPORT MODEL	NASA TM X-1223 EXPERIMENTAL EVALUATION OF SEVERAL ABLATIVE MATERIALS AS NOZZLE SECTIONS OF A STORABLE-PROPELLANT ROCKET ENGINE	NASA TM X-1230 A COMPUTER PROGRAM TO IMPROVE STADAN STATION SCHEDULING	NASA TM X-1243 THE EFFECT OF PROTUBERANCES, CAVITIES, AND ANGLE OF ATTACK ON THE WIND-TUNNEL PRESSURE AND HEAT-TRANSFER DISTRIBUTION FOR THE APOLLO COMMAND MODULE	NASA TM X-1268 HIGH-VACUUM TECHNOLOGY, TESTING, AND MEASUREMENT MEETING- JUNE 8-9, 1965	NASA TM X-1279 AEROBEE 150 STRUCTURAL AND AERODYNAMIC PITCH COUPLING	NASA TM X-135 TRANSONIC FLUTTER CHARACTERISTICS OF A 45(DEGRE) SWEPTBACK WING WITH VARIOUS DISTRIBUTIONS OF BALLAST ALONG THE LEADING EDGE	Next

Bound With Nasa Tm X-1202-1230,1268-1279,Lack No. 1203-13,15-22,24-29,31-42,44-67,69-78

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