SHOCK-FRONT-THICKNESS MEASUREMENTS BY AN ELECTRON BEAM TECHNIQUE

[1] Becker R., 1922, Z PHYS, V8, P321, DOI DOI 10.1007/BF01329605

[2] BURNETT D, 1935, P LOND MATH SOC, V40, P382, DOI DOI 10.1112/PLMS/S2-40.1.382

[3] THE EXPERIMENTAL DETERMINATION OF THE THICKNESS OF A SHOCK FRONT IN A GAS [J]. JOURNAL OF CHEMICAL PHYSICS, 1950, 18 (08) : 1008 - 1018

[4] GILBARG D, 1953, J RATION MECH ANAL, V2, P617

[5] THE PROFILE OF A STEADY PLANE SHOCK WAVE [J]. COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1952, 5 (03) : 257 - 300

[6] GREENE, 1951, J CHEM PHYS, V19, P427

[7] KAPLAN DE, 1955, J APPL PHYS, V26, P639

[8] ON A COMPLETE SOLUTION OF THE ONE-DIMENSIONAL FLOW EQUATIONS OF A VISCOUS, HEAT-CONDUCTING, COMPRESSIBLE GAS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (11): : 674 - &

[9] MOTTSMITH HM, 1951, PHYS REV, V83, P885

[10] Rayleigh, 1910, P R SOC LOND A-CONTA, V84, P247

[1] Becker R., 1922, Z PHYS, V8, P321, DOI DOI 10.1007/BF01329605

[2] BURNETT D, 1935, P LOND MATH SOC, V40, P382, DOI DOI 10.1112/PLMS/S2-40.1.382

[3] THE EXPERIMENTAL DETERMINATION OF THE THICKNESS OF A SHOCK FRONT IN A GAS [J]. JOURNAL OF CHEMICAL PHYSICS, 1950, 18 (08) : 1008 - 1018

[4] GILBARG D, 1953, J RATION MECH ANAL, V2, P617

[5] THE PROFILE OF A STEADY PLANE SHOCK WAVE [J]. COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1952, 5 (03) : 257 - 300

[6] GREENE, 1951, J CHEM PHYS, V19, P427

[7] KAPLAN DE, 1955, J APPL PHYS, V26, P639

[8] ON A COMPLETE SOLUTION OF THE ONE-DIMENSIONAL FLOW EQUATIONS OF A VISCOUS, HEAT-CONDUCTING, COMPRESSIBLE GAS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (11): : 674 - &

[9] MOTTSMITH HM, 1951, PHYS REV, V83, P885

[10] Rayleigh, 1910, P R SOC LOND A-CONTA, V84, P247