cranfield0066

effect joint conduct temperatur thermal stress aerodynam heat skin stiffen combin temperatur thermal stress typic skin stiffen combin winglik structur subject aerodynam heat obtain aid electron differenti analyz variat made aerodynam heat transfer paramet joint conduct paramet ratio skin width skin thick result present nondimension form indic decreas joint conduct paramet lower interior averag temperatur ratio increas peak thermal stress ratio skin may consider increas peak stiffen stress ratio increas aerodynam heat transfer paramet decreas interior averag temperatur ratio increas peak skin stress ratio somewhat greatli increas peak stiffen stress ratio increas ratio skin width skin thick produc moder decreas peak skin stress ratio moder increas peak stiffen stress ratio