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Page Title:
Figure 2. Compression Wave Formation |
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|  T-45A/C TS, ADV & IUT Aero-02
High-Speed Flight
FLIGHT MACH IS LESS THAN ONE
Sonic Flow (m = 1)
Flow Accelerates to above Flight Mach
MCRIT = .80 MACH For T-45
Normal Shock Wave
Supersonic
Normal Shock Wave
Supersonic
Flow
Flow
Possible Separation
Subsonic
Subsonic
1
= M 0.83
M 1.2
Oblique
Normal Shock Wave
Supersonic Flow
Shock Wave
Supersonic
Flow
Separation
Separation
Oblique
Supersonic Flow
Normal Shock Wave
Shock Wave
Oblique
Shock Wave
Supersonic Flow
Stagnated
Subsonic Flow
Subsonic
Flow
Separation
Subsonic
Flow
Supersonic Flow
Oblique
Shock Wave
Bow Wave
Figure 2: COMPRESSION WAVE FORMATION
(9-99) Original
Page 2-7
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