Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /
|Main Author:||Mohn, Larry Wayne.|
Washington, D.C. : National Aeronautics and Space Administration ; 1975]
Jet transports /
Design and construction.
Airplanes > Airplanes / Nacelles.
"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
vi, 87 p. :
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||University of Illinois at Urbana-Champaign|