Terminal-shock and restart control of a Mach 2.5, axisymmetric, mixed-compression inlet with 40-percent internal contraction / by Robert J. Baumbick, Robert E. Wallhagen, and Robert C. Seidel.

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Bibliographic Details
Main Author:	Baumbick, Robert J.
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Wallhagen, Robert E., Seidel, Robert C.
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-2992.
Subjects:	Airplanes > Turbojet engines > Air intakes > Automatic control. Airplanes > Turbofan engines. Aerodynamics, Supersonic. Air ducts > Aerodynamics.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:2992
NAS 1.15:2992	Available Place a Hold