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Research on the sonic boom problem. Part 2: Flow field measurement in wind tunnel and calculation of second order F-function [NASA CR-2340]

By: Landahl, M.

Contributor(s): Soerensen, H | Hilding, L.

Material type: materialTypeLabel

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Nasa Washington, D. C. 1973Description: 107p.Subject(s): Sonic boom--Research

Contents:

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-2340 (Browse shelf)	Not for loan		TR101616(R)

Total holds: 0

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Previous	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]	NASA CR-2341 Quantitative understanding of explosive stimulus transfer [NASA CR-2341]	NASA CR-2343 The radiometer transfer function for the AAFE composite two-frequency radiometer scatterometer. M.S. Thesis - Pennsylvania Univ. [NASA CR-2343]	Next

NASA technical report

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