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TRANSITION CHARACTERISTICS OF A VTOL AIRCRAFT POWERED BY FOUR DUCTED TANDEM PROPELLERS

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BookPublisher: Nasa, Washington, D.C. 1964Description: 55.DDC classification: NASA | TN D-2254

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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-2254 (Browse shelf)	Not for loan		TR13795

Total holds: 0

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Previous	NASA TN D-2250 INSTRUMENTATION FOR FAR ULTRAVIOLET ROCKET SPECTROPHOTOMETRY	NASA TN D-2252 A FLIGHT STUDY OF MANUAL BLIND LANDING PERFORMANCE USING CLOSED CIRCUIT TELEVISION DISPLAYS	NASA TN D-2253 ANALYTICAL EVALUATION OF POSSIBLE NONCRYOGENIC PROPELLANTS FOR ELECTROTHERMAL THRUSTORS	NASA TN D-2254 TRANSITION CHARACTERISTICS OF A VTOL AIRCRAFT POWERED BY FOUR DUCTED TANDEM PROPELLERS	NASA TN D-2255 THE ADAPTIVE DYNAMIC RESPONSE CHARACTERISTICS OF THE HUMAN OPERATOR IN SIMPLE MANUAL CONTROL	NASA TN D-2256 FORMATION OF DETONATION WAVES IN HYDROGEN-OXYGEN MIXTURES FROM 02 TO 2 ATMOSPHERES INITIAL PRESSURE IN A 54-METER LONG TUBE	NASA TN D-2257 CODING AN ANALOG VARIABLE FOR CONSTANT PERCENTAGE ERROR	Next

Bound With Nasa Tn D-2251-2253,2255-2260

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