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.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:2554
NAS 1.26:2554	Available Place a Hold