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SUPERSONIC ASYMMETRIC FLUTTER AND DIVERGENCE OF TRUNCATED CONICAL SHELLS WITH RING-SUPPORTED EDGES

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BookPublisher: Nasa, Washington, D.C. 1971Description: 24.DDC classification: NASA | TN D-6223 -

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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-6223 - (Browse shelf)	Not for loan		TR9569

Total holds: 0

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Previous	NASA TN D-622 AERODYNAMIC CHARACTERISTICS AT LOW SPEED OF A REENTRY6 CONFIGURATION HAVING RIGID RESTRACTABLE CONICAL LIFTING SURFACES	NASA TN D-6221 - CALCULATION BY A FINITE-DIFFERENCE METHOD OF SUPERSONIC TURBULENT BOUNDARY LAYERS WITH TANGENTIAL SLOT INJECTION	NASA TN D-6222 - EFFECT OF ENGINE POSITION AND HIGH-LIFT DEVICES ON AERODYNAMIC CHARACTERISTICS OF AN EXTERNAL-FLOW JET-FLAP STOL MODEL	NASA TN D-6223 - SUPERSONIC ASYMMETRIC FLUTTER AND DIVERGENCE OF TRUNCATED CONICAL SHELLS WITH RING-SUPPORTED EDGES	NASA TN D-6224 - EXPERIMENTAL INVESTIGATION OF THREE BALLOON-TYPE ENCLOSURES FOR THERMAL CONTROL OF SETELLITES	NASA TN D-6225 - SIMULATOR STUDY OF FLIGHT CHARACTERISTICS OF A JET-FLAP STOL TRANSPORT AIRPLANE DURING APPROACH AND LANDING	NASA TN D-6226 - REFERENCE SYSTEM CHARACTERISTICS FOR MANNED STOPOVER MISSIONS TO MARS AND VENUS	Next

Bound With Nasa Tn D-6220-29

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