NASA-TN-D-6348
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- 1.62 MB File Size
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- June 16, 2016 Create Date
- June 16, 2016 Last Updated
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Comparison of Wind Tunnel and Flight Measured Base Pressure from the Sharp Leading Edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers From 1.5 to 5.0
| File | Action |
|---|---|
| NASA-TN-D-6348 Comparison of Wind Tunnel and Flight Measured Base Pressure from the Sharp Leading Edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach.pdf | Download |
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