Question Cagtegory: Aeronautics
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Supersonic flow has a Mach number
- 499 views
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- 2 votes
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The temperature and pressure at the stagnation point of a high speed missile are \({934^ \circ }\) R and 7.8 atm, …
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What are supersonic airplanes?
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What is the function of rudder in the aircraft?
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What determines the length of airport runway?
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What is the difference between taxiway and runway?
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What are sonic booms and Mach cone?
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What are indicated, calibrated, equivalent and true airspeed ?
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What is ground effect ? How does ground effect affects landing of an airplane?
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What are profile drag, parasite drag, induced drag and wave drag?
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