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About Local Flow Measurements at the Inlet Spike Tip of a mach 3 Supersonic Cruise Airplane
stream Mach numbers from 1. 6 to 3. 0. Local flow angularity, Mach number, free—stream Mach numbers, angle of attack, and angle of sideslip.
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2001 |
| Pages: | 42 |
| Language: | English |
| File Size: | 1.54 |
| Format: | |
| Price: | FREE |
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