ON THE PROPAGATION OF WEAK SHOCK WAVES

[1] THE LINEARISED THEORY OF CONICAL FIELDS IN SUPERSONIC FLOW, WITH APPLICATIONS TO PLANE AEROFOILS [J]. AERONAUTICAL QUARTERLY, 1950, 2 (01): : 39 - 84

[2] Lamb H., 1932, HYDRODYNAMICS

[3] LIGHTHILL MJ, 1949, PHILOS MAG, V40, P1202

[4] THE POSITION OF THE SHOCK-WAVE IN CERTAIN AERODYNAMIC PROBLEMS [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1948, 1 (03) : 309 - 318

[5] RAO PS, 1956, AERONAUT QUART, V7, P21

[6] RAO PS, 1956, AERONAUT QUART, V7, P135

[7] THE FLOW PATTERN OF A SUPERSONIC PROJECTILE [J]. COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1952, 5 (03) : 301 - 348

[8] [No title captured]

[1] THE LINEARISED THEORY OF CONICAL FIELDS IN SUPERSONIC FLOW, WITH APPLICATIONS TO PLANE AEROFOILS [J]. AERONAUTICAL QUARTERLY, 1950, 2 (01): : 39 - 84

[2] Lamb H., 1932, HYDRODYNAMICS

[3] LIGHTHILL MJ, 1949, PHILOS MAG, V40, P1202

[4] THE POSITION OF THE SHOCK-WAVE IN CERTAIN AERODYNAMIC PROBLEMS [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1948, 1 (03) : 309 - 318

[5] RAO PS, 1956, AERONAUT QUART, V7, P21

[6] RAO PS, 1956, AERONAUT QUART, V7, P135

[7] THE FLOW PATTERN OF A SUPERSONIC PROJECTILE [J]. COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1952, 5 (03) : 301 - 348

[8] [No title captured]