Catalog Record: Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method | HathiTrust Digital Library

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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.

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Main Author: Mohn, Larry Wayne.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1975]
Subjects: Jet transports > Jet transports / Design and construction.
Aerodynamic load.
Airplanes > Airplanes / Nacelles.
Aerodynamics.
Note: "Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
"July 1975."
Cover title.
Physical Description: vi, 87 p. : ill. ; 27 cm.
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