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Continuoous output tremiminal shock mixed compression inlets evaluated in wind tunnel tests of YF-12 aircfaft inlet [NASA TM X-3144] : National Aeronautics and Space Administration

By: Dustin, Miles O.
Contributor(s): Cole, Gary L | Neiner, George H.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D. C. Ohio 1974Description: 23p.Subject(s): Wind tunnel
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
COMPACT STORAGE (BASEMENT) Reference tr002745
Total holds: 0

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