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FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-44]

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BookPublisher: Washington, D.C. National Aeronautics and Space Administration 1960Description: 127p.Subject(s): Stability and control

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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 41-50	Not for loan		TR010892

Total holds: 0

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Previous	NASA TN [D-7679]	INVESTIGATION AT TRANSONIC SPEEDS TO DETERMINE LATERAL CONTROL EFFECTIVENESS OF BOWLING LATERALLY OVER SURFACES OF 30 DEGREE AND 45 DEGREE SWEPT WINGS [NASA TN D-42]	AN EVALUATION OF LINEARIZED VORTEX THEORY AS APPLIED TO SINGLE AND MULTIPLE ROTORS HOVERING IN AND OUT OF GROUND EFFECT [NASA TN D-43]	FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-44]	FLIGHT INVESTIGATION OF STABILITY AND CONTROL CHARACTERISTICS OF A 1/8-SCALE MODEL OF A TILT-WING VERTICAL-TAKE-OFF-AND-LANDING AIRPLANE [NASA TN D-45]	PLASMA ACCELERATION BY USE OF GUIDED MICROWAVES [NASA TN D-46]	DYNAMIC ANALYSIS OF A SIMPLE REENTRY MANEUVER FOR A LIFTING SATELLITE.[NASA TN D-47]	Next

Bounds vol. contains NASA TN D 41-50

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