cranfield0062

similar solut compress laminar boundari layer heat transfer pressur gradient stewartson transform appli laminar compress boundari layer equat requir similar introduc result set ordinari nonlinear differenti equat previous quot stewartson unsolv requir system prandtl number linear viscos temperatur relat across boundari layer isotherm surfac particular distribut free stream veloc consist similar solut system admit axial pressur gradient arbitrari magnitud heat flux normal surfac arbitrari mach number system differenti equat transform integr system veloc ratio independ variabl system solut found pressur gradient vari caus separ infinit favor gradient wall temperatur absolut zero twice free stream stagnat temperatur solut separ flow also present favor pressur gradient solut uniqu advers pressur gradient solut uniqu two solut infinit famili possibl solut identifi essenti viscid outer edg boundari layer remaind essenti inviscid case favor pressur gradient heat wall veloc within portion boundari layer shown exceed local extern veloc variat reynold analog paramet indic ratio skin friction heat transfer zero surfac temperatur twice free stream stagnat temperatur zero surfac held absolut zero valu appli flat plate