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Effects of angle of attack and bluntness on the shock-layer properties of a 15°cone at Mach number of 10.6 / by Joseph W. Cleary
Author
Cleary, Joseph W.
Published
Washington, D.C. : National Aeronautics and Space Administration, November 1968.
Physical Description
1 online resource (38 pages) : illustrations
Additional Creators
United States. National Aeronautics and Space Administration
Access Online
purl.fdlp.gov
Full Text available online
Availability
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Series
NASA technical note ; D-4909
Restrictions on Access
Free-to-read Unrestricted online access
Report Numbers
NAS 1.14:D-4909
Subject(s)
Mach number
Aerodynamics
Conical shells
Shock (Mechanics)
Note
"November 1968."
Bibliography Note
Includes bibliographical references (page 11).
Action Note
committed to retain. Federal Depository Library Program (FDLP). For information on our retention commitment, please contact Microforms and Government Information.
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| catkey: 33846782