| 1. | No variation of density, speed of sound and Mach number is allowed.
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| 2. | It was repowered to to give Mach number 1 capability in 1945.
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| 3. | The wing-and tail-thickness ratio was also reduced to increase the critical Mach number.
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| 4. | The true airspeed corresponding to the critical Mach number generally decreases with altitude.
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| 5. | This graph shows relationship between shock loss coefficient and Rotor inlet Mach number
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| 6. | Mach number, Reynolds number ) are already linked in the text.
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| 7. | The optimum flight Mach number for transition on the J58 was about Mach 2.
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| 8. | This is a reasonable assumption when the Mach Number is less than about 0.3.
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| 9. | For a supersonic flight Mach number, acceleration is typically achieved via a convergent-divergent nozzle.
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| 10. | The second difficulty occurs when the aircraft Mach number changes.
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