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WIND TUNNEL INVESTIGATION OF TAIL BUFFET AT SUBSONIC AND TRANSONIC SPEEDS EMPLOYING A DYNAMIC ELASTIC AIRCRAFT MODEL.[NASA TN D-1362]

By: Rigby, R. N.

Contributor(s): Cornette, E. S.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1962Description: 43p.

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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-1362 (Browse shelf)	Not for loan		TR7458

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

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Previous	NASA TN D-1348 SPACECRAFT INFORMATION SYSTEMS.	NASA TN D-1349 THE DISTRIBUTION OF SMALL INTERPLANETARY DUST PARTICLES IN THE VICINITY OF EARTH	NASA TN D-1350 COMPUTATION OF THE PERTURBATIONS OF NEARLY CIRCULAR ORBITS, USING A NON-SINGULAR SET OF VECTORIAL ELEMENTS.	NASA TN D-1362 WIND TUNNEL INVESTIGATION OF TAIL BUFFET AT SUBSONIC AND TRANSONIC SPEEDS EMPLOYING A DYNAMIC ELASTIC AIRCRAFT MODEL.[NASA TN D-1362]	NASA TN D-1363 WIND-TUNNEL INVESTIGATION OF THE DRAG AND STATIC STABILITY CHARACTERISTICS OF FOUR HELICOPTER FUSELAGE MODELS.	NASA TN D-1364 A WIND-TUNNEL INVESTIGATION OF TEHE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF TWO FULL-SCALE HELICOPTER FUSELAGE MODELS WITH APPENDAGES.	NASA TN D-1365 LONGLITUDINAL STABILITY AND CONTROL OF A TILT-WING VTOL AIRCRAFT MODEL WITH RIGID AND FLAPPING PROPELLER BLADES.	Next

Bounds With NASA TN D 1361-1370

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