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NASA Technical Note: AERODYNAMIC CHARACTERISTICS OF TWIN-PROPELLER DEFLECTED-SLIPSTREAM STOL AIRPLANE MODEL WITH BOUNDARY-LAYER CONTROL ON INVERTED V-TAIL

By: Margason, Richard J.

Contributor(s): Gentry, Garl L.

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BookSeries: NASA Technical Note ; National Aeronautics and Space Administration. Publisher: Washington, D.C. NASA 1968Description: 179p.Subject(s): Small Deflected-Slipstream Short Take-Off and Landing (STOL)

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-4856	Not for loan		TR7626

Total holds: 0

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Previous	Theoretical nitric oxide production incidential to autoignition and combustion of several fuels homogeneously dispersed in air under some typical hypersonic flight conditions [NASA CR-2454-2458] [BV contains NASA CR-2454-2458]	Modern sampled-data control theory [NASA CR-2457] [Bound contains NASA CR-2454-2458]	Measurements of the dielectric properties of sea water at 1.43GHz [NASA CR-2458] [BV contains NASA CR-2454-2458]	NASA Technical Note: AERODYNAMIC CHARACTERISTICS OF TWIN-PROPELLER DEFLECTED-SLIPSTREAM STOL AIRPLANE MODEL WITH BOUNDARY-LAYER CONTROL ON INVERTED V-TAIL	NASA Technical Note: ITERATED COMMUTATORS AND FUNCTIONS OF OPERATORS	NASA Technical Note: CRITICAL-SPEED ANALYSIS OF RIGID ROTORS ON FLEXIBLE FOUNDATIONS	NASA Technical Note: MATHEMATICAL MODEL FOR CALCULATING THE FLIGHT DYNAMICS OF A GENERAL PARACHUTE-PAYLOAD SYSTEM	Next

Bound Volume No.101116 Contents TR 7622-7630

Technical Note D-4851-4860

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