Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /
L.W. Mohn.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration ; 1975]
- Note
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"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
"July 1975."
Cover title.
- Physical Description
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vi, 87 p. :
ill. ;
27 cm.
Viewability
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University of Illinois at Urbana-Champaign
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