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THE EFFECT ON THE DRAG OF A WING-BODY COMBINATION OF MOMENT-OF-AREA-RULE MODIFICATIONS WITH PODS DUCTED TO SIMULATE ENGINE NACELLES

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BookPublisher: Nasa, Washington, D.C. 1960Description: 15.DDC classification: NASA | TN D-308

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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-308 (Browse shelf)	Not for loan		TR15953

Total holds: 0

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Previous	NASA TN D-3068 EVALUATION OF A SUBSCALE INTERNALLY INSULATED FIBER-GLASS PROPELLANT TANK FOR LIQUID HYDROGEN	NASA TN D-3069 SEPARATION TRAJECTORY CHARACTERISTICS RESULTING FROM SEPARATING TWO VEHICLES IN NEAR-EARTH ORBITS	NASA TN D-3070 OPERATIONAL AND PERFORMANCE CHARACTERISTICS OF THE X-15 SPHERICAL, HYPERSONIC FLOW-DIRECTION SENSOR	NASA TN D-308 THE EFFECT ON THE DRAG OF A WING-BODY COMBINATION OF MOMENT-OF-AREA-RULE MODIFICATIONS WITH PODS DUCTED TO SIMULATE ENGINE NACELLES	NASA TN D-3097 CRIRICAL MASS STUDIES WITH NASA ZERO POWER REACTOR II.	NASA TN D-310 TESTS OF AN AREA SUCTION FLAP ON AN NACA 64A010 AIRFOIL AT HIGH SUBSONIC SPEEDS	NASA TN D-3112 A STUDY OF GEMINI-AGENA DOCKING USING A FIXED-BASE SIMULATOR EMPLOYING A CLOSED-CIRCUIT TELEVISION SYSTEM	Next

Bound With Nasa Tn D-301-07,309-10

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