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A numerical method for calculating the flat-plate pressure distribution on supersonic wings of supersonic wings of arbitrary planform. [NASA TN D-2570]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C NASA 1965Description: 23p.Subject(s): Arbitrary

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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 TN D-2570 (Browse shelf)	Not for loan		TR83084

Total holds: 0

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