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FLUTTER OF CURVED AND FLAT SANDWICH PANELS SUBJECTED TO SUPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1964Description: 13.DDC classification: NASA | TN D-2192 -

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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-2192 - (Browse shelf)	Not for loan		TR9932

Total holds: 0

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Previous	NASA TN D-2189 DESCRIPTION OF VEHICLE SYSTEM AND FLIGHT TESTS OF NIN TRAILBLAZER I REENTRY PHYSICS RESEARCH VEHICLES	NASA TN D-219 A THREE-STAGES SOLID-FUEL SOUNDING ROCKET SYSTEM SUITABLE FOR RESEARCH AT ALTITUDES NEAR 200 NAUTICAL MILES.	NASA TN D-2190 SUPERSONIC LONGITUDINAL STABILITY CHARACTERISTICS OF THE TWO FINAL STAGES OF A FOUR-STAGE LAUNCH VEHICLE	NASA TN D-2192 - FLUTTER OF CURVED AND FLAT SANDWICH PANELS SUBJECTED TO SUPERSONIC FLOW	NASA TN D-2193 - FFECTS OF LAMINAR-BOUNDARY -LAYER DISPLACEMENT ON A HEMISPHERE IN HELIUM FLOW	NASA TN D-2194 - THE ECHO I INFLATION SYSTEM	NASA TN D-2196 - EFFECTS OF WEIGHT, DENSITY AND HEAT LOAD ON THERMAL-SHIELDING PERFORMANCE OF PHENOLIC NYLON	Next

Bound With Nasa Tn D-2191-2200

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