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impact pressure : ウィキペディア英語版
impact pressure
In compressible fluid dynamics, impact pressure (dynamic pressure) is the difference between total pressure (also known as pitot pressure or stagnation pressure) and static pressure.〔(DoD and NATO definition of impact pressure ) Retrieved on 2008-10-01〕 〔(The Free Dictionary ) Retrieved on 2008-10-01〕 In aerodynamics notation, this quantity is denoted as q_c or Q_c.
When input to an airspeed indicator, impact pressure is used to provide a calibrated airspeed reading. An air data computer with inputs of pitot and static pressures is able to provide a Mach number and, if static temperature is known, true airspeed.
Some authors in the field of compressible flows use the term ''dynamic pressure'' or ''compressible dynamic pressure'' instead of ''impact pressure''.〔Clancy, L.J., ''Aerodynamics'', Section 3.12 and 3.13〕〔"the dynamic pressure is equal to ''half rho vee squared'' only in incompressible flow."
Houghton, E.L. and Carpenter, P.W. (1993), ''Aerodynamics for Engineering Students'', Section 2.3.1〕
==Isentropic flow==
In isentropic flow the ratio of total pressure to static pressure is given by:〔
\frac = \left(1+ \frac M^2 \right)^\tfrac
where:

P_t is total pressure
P is static pressure
\gamma\; is the ratio of specific heats

M\; is the freestream Mach number
Taking \gamma\; to be 1.4, and since \;P_t=P+q_c
\;q_c = P\left(M^2 \right)^\tfrac-1\right )
Expressing the incompressible dynamic pressure as \;\tfrac\gamma PM^2 and expanding by the binomial series gives:
\;q_c=q \left(1 + \frac + \frac + \frac ... \right)\;
where:
\;q is dynamic pressure

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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