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EFFECTS OF AIRCRAFT RELATIVE DENSITY ON SPIN AND RECOVERY CHARACTERISTICS OF SOME CURRENT CONFIGURATIONS

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BookPublisher: Nasa, Washington, D.C. 1965Description: 38.DDC classification: NASA | TN D-2243

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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-2243 (Browse shelf)	Not for loan		TR16178

Total holds: 0

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Previous	NASA TN D-2239 AERODYNAMIC AND ROCKET BRAKING OF BLUNT NONLIFTING VEHICLES ENTERING THE EARTH`S ATMOSPHERE AT VERY HIGH SPEEDS	NASA TN D-2240 INVESTIGATION OF MECHANISMS OF POTENTIAL AIRCRAFT FUEL TANK VENT FIRES AND EXPLOSIONS CAUSED BY ATMOSPHERIC ELECTRICITY	NASA TN D-2242 HIGH-SPEED PHOTOGRAPHIC INVESTIGATION OF THE FORMATION OF DETONATION WAVES IN A STOICHIOMETRIC HYDROGEN-OXYGEN MIXTURE	NASA TN D-2243 EFFECTS OF AIRCRAFT RELATIVE DENSITY ON SPIN AND RECOVERY CHARACTERISTICS OF SOME CURRENT CONFIGURATIONS	NASA TN D-2244 RADAR INVESTIGATION OF METEORS AT HIGH RATES OF DETECTION	NASA TN D-2245 FREQUENCIES AND MODES OF VIBRATION OF BUCKLED CIRCULAR PLATES	NASA TN D-2246 THEORETICAL STUDIES OF A RADIATION-BALANCE	Next

Bound With Nasa Tn D-2241-42,2244-50

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