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ANALYSIS OF WING SLIPSTREAM FLOW INTRACTION [NASA CR-1632]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. NASA 1970Description: iv, 145p.Subject(s): Wing slipstreamDDC classification: NASA | CR-1632

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1632 (Browse shelf)	Not for loan		TR8206

Total holds: 0

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Previous	NASA CR-1621 Theoretical frequency response function and power spectra of the XB-70 response to atmospheric turbulence [NASA CR-1621)	NASA CR-1622 Perturbation theory based on life transforms and its application to the stability of motion near sun-perturbed earth-moon triangular liberation points [NASA CR-1622]	NASA CR-1631 XB-70 flight test data comparisons with simulation predictions of inlet unstart and buzz[NASA CR-1631]	NASA CR-1632 ANALYSIS OF WING SLIPSTREAM FLOW INTRACTION [NASA CR-1632]	NASA CR-1633 PREPARATION AND CHARACTERIZATION OF LOW DP END-CAPPED PYRRONE MOLDINGS [NASA CR-1633]	NASA CR-1634 DATA DISPLAY AND ANALYSIS {NASA CR-1634]	NASA CR-1635 JUDGEMENT TEST OF FLYOVER NOISE FROM VARIOUS AIRCRAFT [NASA CR-1635]	Next

Bound With NASA CR-1631-40 (Bound Acc. no.101540)

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