FLOW NONUNIFORMITY IN SHOCK TUBES OPERATING AT MAXIMUM TEST TIMES

[1] CAMAC M, 1966, RAREFIED GAS DYNAMIC

[2] SHOCK-TUBE PERFORMANCE AT LOW INITIAL PRESSURE [J]. PHYSICS OF FLUIDS, 1959, 2 (02) : 207 - 216

[3] FOX JN, 7 P INT C ION PHEN G

[4] TEST TIME IN LOW-PRESSURE SHOCK TUBES [J]. PHYSICS OF FLUIDS, 1963, 6 (09) : 1201 - 1214

[5] SHOCK TUBE TEST TIME LIMITATION DUE TO TURBULENT-WALL BOUNDARY LAYER [J]. AIAA JOURNAL, 1964, 2 (01) : 84 - 93

[6] MIRELS H, 1957, NACA4021 TECHN NOT

[7] PUKHNACHEV VV, 1963, J PRIKL MEKH TEKH FI, P66

[8] ON FLOW DURATION IN LOW-PRESSURE SHOCK TUBES [J]. PHYSICS OF FLUIDS, 1960, 3 (06) : 835 - 842

[9] 1953, NACA1135 TECHN REP

[1] CAMAC M, 1966, RAREFIED GAS DYNAMIC

[2] SHOCK-TUBE PERFORMANCE AT LOW INITIAL PRESSURE [J]. PHYSICS OF FLUIDS, 1959, 2 (02) : 207 - 216

[3] FOX JN, 7 P INT C ION PHEN G

[4] TEST TIME IN LOW-PRESSURE SHOCK TUBES [J]. PHYSICS OF FLUIDS, 1963, 6 (09) : 1201 - 1214

[5] SHOCK TUBE TEST TIME LIMITATION DUE TO TURBULENT-WALL BOUNDARY LAYER [J]. AIAA JOURNAL, 1964, 2 (01) : 84 - 93

[6] MIRELS H, 1957, NACA4021 TECHN NOT

[7] PUKHNACHEV VV, 1963, J PRIKL MEKH TEKH FI, P66

[8] ON FLOW DURATION IN LOW-PRESSURE SHOCK TUBES [J]. PHYSICS OF FLUIDS, 1960, 3 (06) : 835 - 842

[9] 1953, NACA1135 TECHN REP