ATTENUATION IN THE SHOCK TUBE .1. LAMINAR FLOW

[1] Bannister FK., 1948, P I MECH ENG, V159, P269, DOI [10.1243/PIME_PROC_1948_159_024_02, DOI 10.1243/PIME_PROC_1948_159_024_02]

[2] BLEAKNEY, 1949, REV SCI INSTRUM, V20, P807

[3] BLEAKNEY W, COMMUNICATION

[4] TEMPERATURE AND VELOCITY PROFILES IN THE COMPRESSIBLE LAMINAR BOUNDARY LAYER WITH ARBITRARY DISTRIBUTION OF SURFACE TEMPERATURE [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (09): : 547 - 565

[5] CORRSIN S, 1949, VISCOUS FLUID FLOW

[6] COURANT R, 1948, SUPERSONIC FLOW SHOC, P92

[7] DONALDSON C, 1949, NACA TN1942

[8] ATTENUATION IN THE SHOCK TUBE [J]. JOURNAL OF APPLIED PHYSICS, 1953, 24 (03) : 360 - 363

[9] EMRICH RJ, 1948, VELOCITY MEASUREMENT

[10] SHOCK-WAVE AND BOUNDARY-LAYER PHENOMENA NEAR A FLAT SURFACE [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1947, 190 (1020): : 1 - &

[1] Bannister FK., 1948, P I MECH ENG, V159, P269, DOI [10.1243/PIME_PROC_1948_159_024_02, DOI 10.1243/PIME_PROC_1948_159_024_02]

[2] BLEAKNEY, 1949, REV SCI INSTRUM, V20, P807

[3] BLEAKNEY W, COMMUNICATION

[4] TEMPERATURE AND VELOCITY PROFILES IN THE COMPRESSIBLE LAMINAR BOUNDARY LAYER WITH ARBITRARY DISTRIBUTION OF SURFACE TEMPERATURE [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (09): : 547 - 565

[5] CORRSIN S, 1949, VISCOUS FLUID FLOW

[6] COURANT R, 1948, SUPERSONIC FLOW SHOC, P92

[7] DONALDSON C, 1949, NACA TN1942

[8] ATTENUATION IN THE SHOCK TUBE [J]. JOURNAL OF APPLIED PHYSICS, 1953, 24 (03) : 360 - 363

[9] EMRICH RJ, 1948, VELOCITY MEASUREMENT

[10] SHOCK-WAVE AND BOUNDARY-LAYER PHENOMENA NEAR A FLAT SURFACE [J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1947, 190 (1020): : 1 - &