Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /

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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Bibliographic Details
Online Access: Search for the full-text version of this title in HathiTrust
Main Author: Mohn, Larry Wayne
Corporate Authors: Boeing Commercial Airplane Company, Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], [1975]
Series:NASA contractor report ; NASA CR-2554.
Subjects:
Aerodynamics.
Airplanes > Nacelles.
Aerodynamic load.
Jet transports > Design and construction.
Description
Item Description:Cover title.
"July 1975."
"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center."
Physical Description:vi, 87 pages : illustrations ; 27 cm.
Bibliography:Includes bibliographical references (page 87)

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