INVESTIGATION OF THE SHOCK-TUBE BOUNDARY LAYER BY A TRACER METHOD

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

[2] BELL S, 1955, HE150133 U CALIF I E

[3] BERSHADER D, 1956, 1122 PRINC U DEP PHY

[4] BOURAT JM, 1949, PUBL SCI TECH MINIST, V226

[5] CADY WM, 1954, HIGH SPEED AERODYNAM, V9, P142

[6] CHABAI AJ, 1958, 12 LEH U CHAB I TECH

[7] CHEN CJ, 1960, 15 LEH U DEP PHYS TE

[8] EMMONS LB, 1957, THESIS LEHIGH U

[9] An examination of turbulent flow with an ultramicroscope [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-CONTAINING PAPERS OF A MATHEMATICAL AND PHYSICAL CHARACTER, 1932, 135 (828) : 656 - 677

[10] GOLDSTEIN S, 1938, MODERN DEV FLUID DYN, V2, P626

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

[2] BELL S, 1955, HE150133 U CALIF I E

[3] BERSHADER D, 1956, 1122 PRINC U DEP PHY

[4] BOURAT JM, 1949, PUBL SCI TECH MINIST, V226

[5] CADY WM, 1954, HIGH SPEED AERODYNAM, V9, P142

[6] CHABAI AJ, 1958, 12 LEH U CHAB I TECH

[7] CHEN CJ, 1960, 15 LEH U DEP PHYS TE

[8] EMMONS LB, 1957, THESIS LEHIGH U

[9] An examination of turbulent flow with an ultramicroscope [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-CONTAINING PAPERS OF A MATHEMATICAL AND PHYSICAL CHARACTER, 1932, 135 (828) : 656 - 677

[10] GOLDSTEIN S, 1938, MODERN DEV FLUID DYN, V2, P626