HYPERSONIC MERGED STAGNATION SHOCK LAYERS .1. ADIABATIC WALL CASE

[1] AHOUSE DR, 1969, AIAA69656 PAP

[2] CHENG HK, 1961, 1961 P HEAT TRANSF F, P161

[3] COMPUTATION OF NONEQUILIBRIUM MERGED STAGNATION SHOCK LAYERS BY SUCCESSIVE ACCELERATED REPLACEMENT [J]. AIAA JOURNAL, 1971, 9 (02) : 262 - +

[4] HEAT TRANSFER TO A HEMISPHERE-CYLINDER AT LOW REYNOLDS NUMBERS [J]. AIAA JOURNAL, 1963, 1 (03) : 665 - 672

[5] JAIN AC, 1972, REPT MINISTRY DEFENC

[6] JAIN AC, 1968, SUM P SEM FLUID DYN, P65

[7] JAIN AC, 1973, AIAA73639 PAP

[8] HYPERSONIC VISCOUS FLOW NEAR THE STAGNATION STREAMLINE OF A BLUNT BODY .2. 3RD-ORDER BOUNDARY-LAYER THEORY AND COMPARISON WITH OTHER METHODS [J]. AIAA JOURNAL, 1964, 2 (11) : 1898 - 1906

[9] HYPERSONIC VISCOUS FLOW NEAR THE STAGNATION STREAMLINE OF A BLUNT BODY .1. A TEST OF LOCAL SIMILARITY [J]. AIAA JOURNAL, 1964, 2 (11) : 1892 - 1897

[10] LEVINSKY FS, 1962, HYPERSONIC FLOW RESE

[1] AHOUSE DR, 1969, AIAA69656 PAP

[2] CHENG HK, 1961, 1961 P HEAT TRANSF F, P161

[3] COMPUTATION OF NONEQUILIBRIUM MERGED STAGNATION SHOCK LAYERS BY SUCCESSIVE ACCELERATED REPLACEMENT [J]. AIAA JOURNAL, 1971, 9 (02) : 262 - +

[4] HEAT TRANSFER TO A HEMISPHERE-CYLINDER AT LOW REYNOLDS NUMBERS [J]. AIAA JOURNAL, 1963, 1 (03) : 665 - 672

[5] JAIN AC, 1972, REPT MINISTRY DEFENC

[6] JAIN AC, 1968, SUM P SEM FLUID DYN, P65

[7] JAIN AC, 1973, AIAA73639 PAP

[8] HYPERSONIC VISCOUS FLOW NEAR THE STAGNATION STREAMLINE OF A BLUNT BODY .2. 3RD-ORDER BOUNDARY-LAYER THEORY AND COMPARISON WITH OTHER METHODS [J]. AIAA JOURNAL, 1964, 2 (11) : 1898 - 1906

[9] HYPERSONIC VISCOUS FLOW NEAR THE STAGNATION STREAMLINE OF A BLUNT BODY .1. A TEST OF LOCAL SIMILARITY [J]. AIAA JOURNAL, 1964, 2 (11) : 1892 - 1897

[10] LEVINSKY FS, 1962, HYPERSONIC FLOW RESE