The unsteady aerodynamics on body are dealt with two quasi steady aerodynamics theories(i.e. slender body method and subsection aerodynamics derivative method which are applicable to subsonic and supersonic flight conditions).

 
  • 用細長(cháng)體理論和氣動(dòng)導數方法計算了導彈的非定常氣動(dòng)力 ,兩種方法均適用于亞音速和超音速情況。
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