CAJ | 학술논문

为准确预测高超声速飞行器翼面的热环境以利于飞行器的设计。通过数值算例验证了基于参考焓法的气动加热工程算法的可行性；提出了一种高超声速飞行器三维翼面的气动加热、辐射换热、瞬态热传导的准定常耦合求解方法，通过与非耦合的气动加热、辐射换热及瞬态热传导方法相比，指出考虑耦合求解的必要性。在飞行器典型弹道飞行条件下，该耦合求解方法考虑气动加热、辐射换热、结构热传导耦合效应，实现了高超声速三维翼面温度的准确预测，该方法可用于高超声速飞行器气动热分析及热防护设计。
위준학예측고초성속비행기익면적열배경이리우비행기적설계。통과수치산례험증료기우삼고함법적기동가열공정산법적가행성；제출료일충고초성속비행기삼유익면적기동가열、복사환열、순태열전도적준정상우합구해방법，통과여비우합적기동가열、복사환열급순태열전도방법상비，지출고필우합구해적필요성。재비행기전형탄도비행조건하，해우합구해방법고필기동가열、복사환열、결구열전도우합효응，실현료고초성속삼유익면온도적준학예측，해방법가용우고초성속비행기기동열분석급열방호설계。
The aerodynamic heating results in the rapid rise of the surface temperature of hypersonic vehicle.In order to accurately predict the thermal environment of vehicle airfoil so as to design vehicle,engineering calculation of aerodynamic heating was proved to be reliable by comparing with numerical simulation.An intergrated coupled simulation in which the aeroheating,radiative heat transfer and structure heat conduction were worked together was obtained.Comparing with the uncoupled simulation,coupled simulation should be payed more attention while calculating aerodynamic heating.Under the conditions of a typical traj ectory,the temperature of three-dimensional airfoils is accurately predicted by the coupled method considering the coupling effect of aeroheating radiative heat-transfer and structure heat-conduction.This method can be appled to arodynamic heating analysis and thermal protection of hypersonic vehicle.