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USE OF SUBSONIC KERNEL FUNCTION IN AN INFLUENCE-COEFFICIENT METHOD OF AEROELASTIC ANALYSIS AND SOME COMPARISONS WITH EXPERIMENT

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BookPublisher: Nasa, Washington, D.C. 1960Description: 86.DDC classification: NASA | TN D-515

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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-515 (Browse shelf)	Not for loan		TR15763

Total holds: 0

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Previous	NASA TN D-5147 FORCES AND MOMENTS DUE TO AIR JETS EXHAUSTING PARALLEL TO LARGE FLAT PLATES IN A NEAR VACUUM	NASA TN D-5148 INVESTIGATION OF A CLASS OF BODIES THAT GENERATE FAR-FIELD SONIC-BOOM SHOCK STRENGTH AND IMPULSE INDEPENDENT OF BODY LENGTH AND VOLUME	NASA TN D-5149 EVALUATION OF A PILOT DESCRIBING FUNCTION METHOD APPLIED TO THE MANUAL CONTROL ANALYSIS OF A LARGE FLEXIBLE BOOSTER	NASA TN D-515 USE OF SUBSONIC KERNEL FUNCTION IN AN INFLUENCE-COEFFICIENT METHOD OF AEROELASTIC ANALYSIS AND SOME COMPARISONS WITH EXPERIMENT	NASA TN D-5150 SIMULATION STUDIES FOR PLANNING AN IN-FLIGHT EXPERIMENT TO DEFINE MANUAL GUIDANCE AND CONTROL TECHNIQUES FOR LARGE LAUNCH VEHICLES	NASA TN D-5152 EFFECT OF OXYGEN CONCENTRATION ON THE PERFORMANCE OF SYNTHETIC PARAFFING OILS IN SHORT TERM BEARING TESTS FROM 400 DEGREE TO 500 DEGREE F.	NASA TN D-5153 Application of Monte Carlo technique for determining maneuvering loads from statistical information on airplane motions [NASA TN D-524]	Next

Bound With Nasa Tn D-511-14,516-20

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