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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.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Cleary, Joseph W., author.
- Series:
- NASA technical note ; D-4909.
- NASA/TN ; D-4909
- Language:
- English
- Subjects (All):
- Mach number.
- Aerodynamics.
- Conical shells.
- Shock (Mechanics).
- aerodynamics.
- Physical Description:
- 1 online resource (38 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, November 1968.
- Notes:
- "November 1968."
- Includes bibliographical references (page 11).
- Description based on online resource, PDF version; title from title page (NASA, viewed on Apr. 23, 2021).
- Other Format:
- Print version: Cleary, Joseph W. Effects of angle of attack and bluntness on the shock-layer properties of a 15℗ʻcone at Mach number of 10.6
- OCLC:
- 1196870103
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