USE OF THE SHOCK TUBE WALL BOUNDARY LAYER IN HEAT TRANSFER STUDIES

[1] BERSHADER D, 1956, LAMINAR BOUNDARY LAY

[2] CROCCO, 1946, MONOGRAPHIE SCI AERO, V13

[3] HARTUNIAN R, 1954, THESIS CORNELL U

[4] HOWARTH, 1953, MODERN DEV FLUID DYN, V1, P400

[5] MIRELS H, 1955, NACATN3401 LAM BOUND

[6] ROTT N, 1955, HEAT T WALLS SHOCK T

[1] BERSHADER D, 1956, LAMINAR BOUNDARY LAY

[2] CROCCO, 1946, MONOGRAPHIE SCI AERO, V13

[3] HARTUNIAN R, 1954, THESIS CORNELL U

[4] HOWARTH, 1953, MODERN DEV FLUID DYN, V1, P400

[5] MIRELS H, 1955, NACATN3401 LAM BOUND

[6] ROTT N, 1955, HEAT T WALLS SHOCK T