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EXPERIMENTAL INVESTIGATION OF OSCILLATORY AERODYNAMIC FORCES,MOMENTS,AND PRESSURES ACTING ON A TAPERED WING OSCILLATING IN PITCH AT MACH NUMBERS FROM 0.40 TO 1.07

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BookPublisher: Nasa, Washington, D.C. 1962Description: 43.DDC classification: NASA | TN D-1236

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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-1236 (Browse shelf)	Not for loan		TR13005

Total holds: 0

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Previous	NASA TN D-1233 EFFECTS OF COUPLING BETWEEN PITCH AND ROLL CONTROL INPUTS ON THE HANDLING QUALITIES OF VTOL AIRCRAFT	NASA TN D-1234 FORCE-TEST INVESTIGATION OF A MODEL OF AN AERIAL VEHICLE SUPPORTED BY FOUR UNSHROUDED PROPELLERS	NASA TN D-1235 FLIGHT-TEST INVESTIGATION OF A MODEL OF AN AERIAL VEHICLE SUPPORTED BY FOUR UNSHROUDED PROPELLERS	NASA TN D-1236 EXPERIMENTAL INVESTIGATION OF OSCILLATORY AERODYNAMIC FORCES,MOMENTS,AND PRESSURES ACTING ON A TAPERED WING OSCILLATING IN PITCH AT MACH NUMBERS FROM 0.40 TO 1.07	NASA TN D-1237 EXPERIMENTAL OBSERVATIONS OF AERODYNAMIC AND HEATING TESTS ON INSULATING HEAT SHIELDS	NASA TN D-1238 INVESTIGATION OF VORTEX MOVEMENTS ABOUT A WING IN INTERMEDIATE AND HIGH SUBSONIC FLOW UNDERGOING A LARGE ANGLE-OF -ATTACK CHANGE IN A BLAST-INDUCED GUST	NASA TN D-1239 AN EXPERIMENTAL STUDY OF THE EFFECT OF DOWNWASH FROM A TWIN-PROPELLER VTOL AIRCRAFT ON SEVERAL TYPES OF GROUND SURFACES	Next

Bound With Nasa Tn D-1231-1235,1237-1240

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