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Flutter analysis and testing of pairs of aerodynamically interfering delta. [NASA CR-2331]

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BookSeries: National Aeronautic and Space Administration (NASA). Publisher: Washington, D.C. Nasa 1973Description: 93p.DDC classification: NASA | CR-2331

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NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA CR-2331 (Browse shelf)	Not for loan		TR10911

Total holds: 0

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Previous	NASA CR-2327 Backscattering from a two-scale rough surface with application to radar sea return. [NASA CR-2327]	NASA CR-2328 Towaed radscat measurements over the sea and their interpretation. [NASA CR-2328]	NASA CR-2329 Atheory of microwave apparent temperature over the ocean. [NASA CR-2329]	NASA CR-2331 Flutter analysis and testing of pairs of aerodynamically interfering delta. [NASA CR-2331]	NASA CR-2339 Research on the sonic boom problem. Part 1: Second-order solutions for the flow field around slender bodies in supersonic flow for sonic boom analysis [NASA CR-2339]	NASA CR-2340 Research on the sonic boom problem. Part 2: Flow field measurement in wind tunnel and calculation of second order F-function [NASA CR-2340]	NASA CR-2340 Research on the sonic boom problem [ Part 2]	Next

NASA technical report

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