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A wind tunnel investigation of panel response to boundary layer pressure fluctuations at mach 1.4 and mach 3.5 (NASA contractor report)

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A wind tunnel investigation of panel response to boundary layer pressure fluctuations at mach 1.4 and mach 3.5 (NASA contractor report) (Unknown Binding)

~ David Alan Bies (Author)

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Product Details

Unknown Binding: 81 pages
Publisher: National Aeronautics and Space Administration (1966)
Language: English
ASIN: B0007HR3U6
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