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FLUTTER DESIGN OF STIFFENED-SKIN PANELS FOR HYPERSONIC AIRCRAFT

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BookPublisher: Nasa, Washington, D.C. 1969Description: 26.DDC classification: NASA | TN D-5555 -

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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-5555 - (Browse shelf)	Not for loan		TR10131

Total holds: 0

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Previous	NASA TN D-5552 - PERFORMANCE ANALYSIS OF THE OPTICAL-MECHANICAL SCANNER AS AN IMAGING SYSTEM FOR PLANETARY LANDERS	NASA TN D-5553 - EXPERIMENTAL DETERMINATION OF EQUIVALENT SOLID BODIES TO REPRESENT JETS EXHAUSTING INTO A MACH 2.20 EXTERNAL STREAM	NASA TN D-5554 - EXPLORATORY HEAT-TRANSFER MEASUREMENTS AT MACH 10 A 7.5(DEGREE) TOTAL-ANGLE CONE DOWNSTREAM OF A REGION OF AIR AND HELIUM TRANSPIRATION COOLING	NASA TN D-5555 - FLUTTER DESIGN OF STIFFENED-SKIN PANELS FOR HYPERSONIC AIRCRAFT	NASA TN D-5556 - SIMPLIFIED BALLISTIC-LIMIT EXPRESSIONS FOR THIN SHEETS	NASA TN D-5557 - SOME FACTORS AFFECTING THE STRESS-CORROSION CRACKING OF TI-6A1-4V ALLOY IN METHANOL	NASA TN D-5558 - AIRBORNE LASER-RADAR STUDIES OF THE LOWER ATMOSPHERE	Next

Bound With Nasa Tn D-5550-69

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