shock stall

名词 n. 动词 v.
中文释义
英 /ˈʃɒk ˌstɔːl/    美 /ˈʃɑk ˌstɔl/

英文释义

名词 n.
  1. A stall (“sudden loss of lift”) caused when the airflow over an aircraft's wings is disturbed by shock waves that occurs at a specific Mach number when the aircraft is accelerating to transonic speeds.
    — When I was down to 32,000 feet the altimeter was spinning merrily and the dive was very steep and I was pulling back on the stick in the usual way due to the change of trim at the shock stall.
动词 v.
  1. Of an aircraft or a component of it: to undergo a shock stall. intransitive
    — The tailplane usually becomes more effective as a stabiliser at high Mach numbers because there are decreases of wing lift-curve slope and rate of change of downwash with mean lift coefficient. The latter effect is mainly due to the wing-root shock stalling at a lower Mach number than the rest of the wing.

词形变化

shock stalls plural shockstall alternative shock-stall alternative shock stalls present,singular,third-person shock stalling participle,present shock stalled participle,past shock stalled past shock-stall alternative

词源

词源 1
The noun is derived from shock + stall (“loss of lift due to an airfoil’s critical angle of attack being exceeded”). The verb is derived from the noun.
词源 2
The noun is derived from shock + stall (“loss of lift due to an airfoil’s critical angle of attack being exceeded”). The verb is derived from the noun.
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