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.
Description
Item Description:Cover title.
"January 1959."
Physical Description:15 pages : 8 illustrations ; 27 cm.
Bibliography:Includes bibliographical references (page 4)

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