APPROXIMATE SOLUTION OF LAMINAR BOUNDARY-LAYER EQUATIONS WITH MASS TRANSFER

[1] BETHEL H, 1967, ARL670045 AER RES LA

[2] BETHEL HE, 1966, THESIS PURDUE U

[3] BETHEL HE, 1966, ARL660090 AER RES LA

[4] VISCOUS FLOW PAST A FLAT PLATE WITH UNIFROM INJECTION [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1965, 284 (1398) : 370 - +

[5] Dorodnitsyn A. A., 1962, ADVANCES AERONAUTICA, V3, P207

[6] Finlayson A., 1966, APPL MECH REV, V19, P735

[7] IGLISH R, 1949, TM1205 NACA

[8] NUMERICAL SOLUTION OF BOUNDARY-LAYER EQUATIONS [J]. AIAA JOURNAL, 1967, 5 (07) : 1231 - &

[9] SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS .1. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY-LAYER-SHOCK-WAVE INTERACTIONS [J]. AIAA JOURNAL, 1964, 2 (11) : 1907 - 1920

[10] NIELSEN JN, 1965, TR65107 AIR FORC FLI

[1] BETHEL H, 1967, ARL670045 AER RES LA

[2] BETHEL HE, 1966, THESIS PURDUE U

[3] BETHEL HE, 1966, ARL660090 AER RES LA

[4] VISCOUS FLOW PAST A FLAT PLATE WITH UNIFROM INJECTION [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1965, 284 (1398) : 370 - +

[5] Dorodnitsyn A. A., 1962, ADVANCES AERONAUTICA, V3, P207

[6] Finlayson A., 1966, APPL MECH REV, V19, P735

[7] IGLISH R, 1949, TM1205 NACA

[8] NUMERICAL SOLUTION OF BOUNDARY-LAYER EQUATIONS [J]. AIAA JOURNAL, 1967, 5 (07) : 1231 - &

[9] SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS .1. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY-LAYER-SHOCK-WAVE INTERACTIONS [J]. AIAA JOURNAL, 1964, 2 (11) : 1907 - 1920

[10] NIELSEN JN, 1965, TR65107 AIR FORC FLI