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HYPERSONIC FLUTTER ANALYSIS USING MEASURED STATIC AERODYNAMIC DERIVATIVES, AND COMPARISON WITH EXPERIMENT [NASA TN D-5233]

By: Goetz, Robert C.

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BookSeries: Naational Aeronautics and Space Administration ; NASA Technical note. Publisher: Washington, D.C. Naational Aeronautics and Space Administration 1969Description: 51p.Subject(s): Aerodynamic

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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-5233	Not for loan		TR009542

Total holds: 0

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Previous	Cavitation and noncovinatinal performance of an 80.6 degree flat platehelical inducer at three rotational speeds [NASA TN D-1439]	on the effct of heat additio in the empirical correlation of void fractions for steam water flow [NASA TN [D-1440]	WIND-TUNNEL INVESTIGATION OF STEADY-STATE AERODYNAMICS OF A COMPOSITE-LIFT VTOL AIRCRAFT MODEL [NASA TN D-5232]	HYPERSONIC FLUTTER ANALYSIS USING MEASURED STATIC AERODYNAMIC DERIVATIVES, AND COMPARISON WITH EXPERIMENT [NASA TN D-5233]	CALORIMETRIC EVALUATION OF THREE 1.5-METER-DIAMETER INFLATABLE RIGIDIZED SOLAR CONCENTRATORS [NASA TN D-5243]	SIMULATION OF GEMINI EXTRAVEHICULAR TASKS BY NEUTRAL-BUOYANCY [NASA TN D-5235]	ANALYTICAL INVESTIGATION OF AN INFLATABLE LANDING SYSTEM HAVING OMNIDIRECTIONAL AND MULTIPLE-IMPACT CAPABILITIES [NASA TN D-5236]	Next

Bound With Nasa Tn D-5231-40

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