Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds / by Roger Chamberlin.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Chamberlin, Roger
Corporate Authors:	Lewis 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], 1974.
Series:	NASA technical memorandum ; X-3053.
Subjects:	Jet nozzles. Airplanes > Turbojet engines. Drag (Aerodynamics) Aerodynamics, Transonic. Reynolds number. Airplanes > Nacelles. Delta Dart (Jet fighter plane)

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3053
NAS 1.15:3053	Available Place a Hold