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EMPIRICAL METHOD FOR DETERMINING STATIC DISTRIBUTED AERODYNAMIC LOADS ON AXISYMMETRIC MULTISTAGE LAUNCH VEHICLES

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BookPublisher: Nasa, Washington, D.C. 1966Description: 104.DDC classification: NASA | TN D-3283 -

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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-3283 - (Browse shelf)	Not for loan		TR10032

Total holds: 0

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