cranfield0072

boundari layer behind shock thin expans wave move stationari fluid boundari layer behind shock thin expans wave advanc stationari fluid determin laminar turbul boundari layer consid wall surfac temperatur behind wave also investig assumpt thin expans wave valid weak expans becom progress less accur strong expans wave laminar boundari layer problem solv numer integr except weak wave case solv analyt integr karman pohlhausen type solut also obtain provid guid determin express accur repres numer data analyt express variou boundari layer paramet present agre numer integr within percent turbul boundari layer problem solv use integr method similar employ solut turbul compress flow semi infinit flat plate fluid veloc rel wall assum seventhpow profil blasiu equat relat turbul skin friction boundari layer thick util form account compress consider heat transfer wall permit wall surfac temperatur behind wave determin wall thick assum greater wall thermal boundari layer thick found wall temperatur uniform function distanc behind wave laminar boundari layer case vari distanc turbul boundari layer case