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Can I read Effects of Aspect Ratio on Air Flow at a High Subsonic Mach Numbers on EtoBox?
Effects of Aspect Ratio on Air Flow at a High Subsonic Mach Numbers by Lindsey, W. F. is a book available to read on EtoBox.
What is Effects of Aspect Ratio on Air Flow at a High Subsonic Mach Numbers about?
Schlieren photographs were used in an investigation to determine the effects of changing the aspect ratio from infinity to two on the air flow past a wing at high subsonic Mach numbers. The results indicated that the decreased effects of compressibility on drag coefficients for the finite wing are produced by a reduction in the compression shock and flow separation
- Author
- Lindsey, W. F.
- Publisher
- National Advisory Committee for Aeronautics, 1948.
- Published
- 1948
- Language
- EN
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