Pressure drag of axisymmetric cowls having large initial lip angles at mach numbers from 1.90 to 4.90 /

Pressure drag of axisymmetric cowls having large initial lip angles at mach numbers from 1.90 to 4.90 / by Nick E. Samanich.

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Bibliographic Details
Main Author: Samanich, Nick E.
Corporate Authors: Lewis Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington [D.C.] : National Aeronautics and Space Administration, [1959]
Series:NASA memorandum ; 1-10-59E.
Subjects:
Drag (Aerodynamics)
Aerodynamics, Supersonic.
Airplanes > Motors > Cowlings.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number: NAS 1.10:1-10-59 E
NAS 1.10:1-10-59 E Available Place a Hold

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