cranfield0097

mix theori interact dissip flow nearli isentrop stream mean simplifi theoret model present paper treat gener class flow problem character interact viscou dissip flow near surfac solid bodi wake outer nearli isentrop stream present extern flow taken plane steadi superson flow make small angl plane surfac plane symmetri although method use extend curv surfac axial symmetr superson flow also subson flow intern dissip flow regard quasi one dimension parallel surfac averag properli defin mean veloc mean temperatur nonuniform actual veloc distribut taken account approxim mean relat mean temperatur mean veloc mix transport momentum outer stream dissip flow consid fundament physic process determin pressur rise support flow aid concept larg number flow problem shown basic similar boundari layer shockwav interact wake flow behind blunt base bodi base pressur problem flow separ overexpand superson nozzl separ wing bodi etc