cranfield0051

theori aircraft structur model subject aerodynam heat extern load problem investig simultan effect transient aerodynam heat extern load aircraft structur purpos determin abil structur withstand flight superson speed studi dimension analys shown construct materi aircraft thermal similar aircraft respect flow heat structur similar aircraft structur model construct temperatur aircraft extern load similar aircraft subject heat cool correctli simul aerodynam heat aircraft except respect angular veloc angular acceler without requir determin heat flux point surfac variat time act aerodynam heat structur model act aircraft determin case zero angular veloc zero angular acceler structur model may subject extern load requir simultan simul stress deform due extern load