One of the most interesting contemporary problems of flight at high supersonic speed is that of heat transfer and its effects on aircraft performance and structure. 當代高超聲速飛行最關(guān)心的問(wèn)題之一，是傳熱及其對飛機結構與性能的影響問(wèn)題。
Bases on the aircraft structure fatigue life theory, consider the characteristics of small UAV, the model of fatigue life prediction for small UVA structure is established. 在飛機結構壽命理論的基礎上，結合小型無(wú)人機機體結構特點(diǎn)，建立了小型無(wú)人機機體壽命分析方法。
