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A WIND-TUNNEL EVALUATION OF ANALYTICAL TECHNIQUES FOR PREDICTING STATIC STABILITY AND CONTROL CHARACTERISTICS OF FLEXIBLE AIRCRAFT

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BookPublisher: Nasa, Washington, D.C. 1972Description: 68.DDC classification: NASA | TN D-6656

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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-6656 (Browse shelf)	Not for loan		TR12290

Total holds: 0

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Previous	NASA TN D-6653 PERFORMANCE OF HIGH-SPEED BALL BEARINGS WITH LEAD-PLATED RETAINERS IN LIQUID HYDROGEN FOR POTENTIAL USE IN A RADIATION ENVIRONMENT	NASA TN D-6654 FAN AND WING FORCE DATA FROM WIND-TUNNEL INVESTIGATION OF A 0.38-METER (15-IN.) DIAMETER VTOL MODEL LIFT FAN INSTALLED IN A TWO-DIMENSIONAL WING	NASA TN D-6655 EXPLORATORY FLIGHT INVESTIGATION OF AIRCRAFT RESPONSE TO THE WING VORTEX WAKE GENERATED BY JET TRANSPORT AIRCRAFT	NASA TN D-6656 A WIND-TUNNEL EVALUATION OF ANALYTICAL TECHNIQUES FOR PREDICTING STATIC STABILITY AND CONTROL CHARACTERISTICS OF FLEXIBLE AIRCRAFT	NASA TN D-6657 COMPARISON OF HINGE MOMENTS FOR A SIMPLE DELTA WING AND A DELTA-WING ORBITOR CONCEPT AT MACH 6	NASA TN D-6658 DESIGN OF A SPECIALIZED COMPUTER FOR ON-LINE MONITORING OF CARDIAC STROKE VOLUME	NASA TN D-6659 PERMEAMETER FOR HIGH-TEMPERATURE MAGNETIC MEASUREMENTS	Next

Bound With Nasa Tn D-6650-55, 6657-59.

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