BOUNDARY-LAYER TRANSITION AND HEAT TRANSFER IN SHOCK TUBES

[1] ASBRIDGE JR, 1959, 14 LEH U I RES TECH

[2] BERSHADER D, 1956, NR061020 PRINC U DEP

[3] Blackman V. H., 1955, II20 PRINC U DEP PHY

[4] BRINICH PF, 1956, NACA TN3659

[5] BRINICH PF, 1954, NACA TN3267

[6] BROMBERG R, 1955, 20280 RAM WOOLDR REP

[7] MEASUREMENT OF WALL TEMPERATURE AND HEAT FLOW IN THESHOCK TUBE [J]. JOURNAL OF APPLIED PHYSICS, 1955, 26 (06) : 779 - 780

[8] CHABAI AJ, 1958, 12 REP

[9] FELDMAN S, 1957, HYPERSONIC GAS DYNAM

[10] GOODERUM PB, 1958, NACA TR4243

[1] ASBRIDGE JR, 1959, 14 LEH U I RES TECH

[2] BERSHADER D, 1956, NR061020 PRINC U DEP

[3] Blackman V. H., 1955, II20 PRINC U DEP PHY

[4] BRINICH PF, 1956, NACA TN3659

[5] BRINICH PF, 1954, NACA TN3267

[6] BROMBERG R, 1955, 20280 RAM WOOLDR REP

[7] MEASUREMENT OF WALL TEMPERATURE AND HEAT FLOW IN THESHOCK TUBE [J]. JOURNAL OF APPLIED PHYSICS, 1955, 26 (06) : 779 - 780

[8] CHABAI AJ, 1958, 12 REP

[9] FELDMAN S, 1957, HYPERSONIC GAS DYNAM

[10] GOODERUM PB, 1958, NACA TR4243