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Flight Theory
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Fundamentals of
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Aircraft Flight Theory
of Aerodynamics
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Flight Theory
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Guide Aircraft
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, Fundamentals of Aerodynamics.pdf Fundamentals of Aerodynamics.pdf Fundamentals of Aerodynamics.pdf
Terms in this set (51)
pitot-static tube compares the total and static pressure to give a reading of dynamic
pressure (indicated airspeed)
indicated airspeed measured as dynamic pressure
calibrated airspeed dynamic pressure with instrument corrections
equivalent airspeed dynamic pressure with instrument and compressibility corrections
true airspeed dynamic pressure with instrument, compressibility, and density and
temperature corrections
decreases mach number ___ across a shockwave
increases static pressure ___ across a shockwave
increases static temperature ___ across a shockwave
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