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EFFECTS OF SIDE-EDGE BOUNDARY CONDITIONS AND TRANSVERSE SHEAR STIFFNESSES ON THE FLUTTER OF ORTHOTROPIC PANELS IN SUPERSONIC FLOW

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BookPublisher: Nasa, Washington, D.C. 1966Description: 40.DDC classification: NASA | TN D-3302

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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-3302 (Browse shelf)	Not for loan		TR12052

Total holds: 0

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Previous	NASA TN D-3299 SALT STRESS CORROSION OF RESIDUALLY STRESSED TI-8A1-MO-1V ALLOY SHEET AFTER EXPOSURE AT ELEVATED TEMPERATURES	NASA TN D-330 AERODYNAMIC PERFORMANCE AND STATIC STABILITY AT MACH NUMBER 3.3 OF AN AIRCRAFT CONFIGURATION EMPLOYING THREE TRIANGULAR WING PANELS AND A BODY OF EQUAL LENGTH	NASA TN D-3300 SUPERSONIC AERODYNAMIC HEATING TESTS ON A LIGHTWEIGHT EXTERNAL INSULATION SYSTEM FOR LIQUID-HYDROGEN TANKS OF BOOST VEHICLES	NASA TN D-3302 EFFECTS OF SIDE-EDGE BOUNDARY CONDITIONS AND TRANSVERSE SHEAR STIFFNESSES ON THE FLUTTER OF ORTHOTROPIC PANELS IN SUPERSONIC FLOW	NASA TN D-3303 THEORETICAL STUDY OF THE EFFECT ON EXPANSION-TUBE PERFORMANCE OF AREA CHANGES AT PRIMARY AND SECONDARY DIAPHRAGM STATIONS	NASA TN D-3304 INVESTIGATION OF THE IMPACT OF HIGH-FINENESS-RATIO PROJECTILES INTO THICK TARGETS	NASA TN D-3305 HUMAN TRANSFER FUNCTIONS IN MULTI-AXIS AND MULTI-LOOP CONTROL SYSTEMS	Next

Bound With Nasa Tn D-3301, 3303-3310.

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