HOT SURFACE - COLD GAS BOUNDARY-LAYER WITH HETEROGENEOUS COMBUSTION

[1] BROWN WB, 1951, TN2479 NACA

[2] CHEN TN, 1965, AIAA PROGR ASTRONAUT, V15, P643

[3] COHEN C, 1955, TN3325 NACA

[4] COMBUSTION AND SUBLIMATION OF CONES SPHERES AND WEDGES AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (11) : 2124 - &

[5] KAUFMAN L, 1969, 5 MAN LABS PROGR REP

[6] MILLER IM, 1966, D3444 TN NASA

[7] STAGNATION-POINT BOUNDARY LAYER WITH LARGE WALL-TO-FREESTREAM ENTHALPY RATIO [J]. AIAA JOURNAL, 1968, 6 (06) : 1105 - &

[8] SUBLIMATION OF GRAPHITE AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (09) : 1635 - &

[9] TRANSPORT AND THERMODYNAMIC PROPERTIES IN A HYPERSONIC LAMINAR BOUNDARY LAYER .2. APPLICATIONS [J]. ARS JOURNAL, 1960, 30 (04): : 329 - 336

[10] TRANSPORT AND THERMODYNAMIC PROPERTIES IN A HYPERSONIC LAMINAR BOUNDARY LAYER PROPERTIES OF THE PURE SPECIES [J]. ARS JOURNAL, 1959, 29 (01): : 39 - 45

[1] BROWN WB, 1951, TN2479 NACA

[2] CHEN TN, 1965, AIAA PROGR ASTRONAUT, V15, P643

[3] COHEN C, 1955, TN3325 NACA

[4] COMBUSTION AND SUBLIMATION OF CONES SPHERES AND WEDGES AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (11) : 2124 - &

[5] KAUFMAN L, 1969, 5 MAN LABS PROGR REP

[6] MILLER IM, 1966, D3444 TN NASA

[7] STAGNATION-POINT BOUNDARY LAYER WITH LARGE WALL-TO-FREESTREAM ENTHALPY RATIO [J]. AIAA JOURNAL, 1968, 6 (06) : 1105 - &

[8] SUBLIMATION OF GRAPHITE AT HYPERSONIC SPEEDS [J]. AIAA JOURNAL, 1965, 3 (09) : 1635 - &

[9] TRANSPORT AND THERMODYNAMIC PROPERTIES IN A HYPERSONIC LAMINAR BOUNDARY LAYER .2. APPLICATIONS [J]. ARS JOURNAL, 1960, 30 (04): : 329 - 336

[10] TRANSPORT AND THERMODYNAMIC PROPERTIES IN A HYPERSONIC LAMINAR BOUNDARY LAYER PROPERTIES OF THE PURE SPECIES [J]. ARS JOURNAL, 1959, 29 (01): : 39 - 45