ON A PERTURBATION THEORY BASED ON THE METHOD OF CHARACTERISTICS

[1] COURANT R, 1948, SUPERSONIC FLOW WAVE, P361

[2] COURANT R, 1937, METHODEN MATH PHYSIK, P322

[3] CRAGGS JW, 1948, P CAMB PHILOS SOC, V44, P360

[4] DONOV A, 1939, IZVESTIA AKADEMIA NA

[5] FOX P, 1953, THESIS MIT

[6] FORMATION AND DECAY OF SHOCK WAVES [J]. COMMUNICATIONS ON APPLIED MATHEMATICS, 1948, 1 (03): : 211 - 245

[7] PLANE JET OF GAS EMITTED FROM A NOZZLE WITH SUPERSONIC VELOCITY [J]. JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN, 1953, 8 (03) : 394 - 399

[8] A NEW APPROACH TO THIN AEROFOIL THEORY [J]. AERONAUTICAL QUARTERLY, 1951, 3 (03): : 193 - 210

[9] LIGHTHILL MJ, 1949, PHILOS MAG, V40, P1179

[10] ON WAVES OF FINITE AMPLITUDE IN DUCTS .1. WAVE FRONTS [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1952, 5 (03) : 257 - 269

[1] COURANT R, 1948, SUPERSONIC FLOW WAVE, P361

[2] COURANT R, 1937, METHODEN MATH PHYSIK, P322

[3] CRAGGS JW, 1948, P CAMB PHILOS SOC, V44, P360

[4] DONOV A, 1939, IZVESTIA AKADEMIA NA

[5] FOX P, 1953, THESIS MIT

[6] FORMATION AND DECAY OF SHOCK WAVES [J]. COMMUNICATIONS ON APPLIED MATHEMATICS, 1948, 1 (03): : 211 - 245

[7] PLANE JET OF GAS EMITTED FROM A NOZZLE WITH SUPERSONIC VELOCITY [J]. JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN, 1953, 8 (03) : 394 - 399

[8] A NEW APPROACH TO THIN AEROFOIL THEORY [J]. AERONAUTICAL QUARTERLY, 1951, 3 (03): : 193 - 210

[9] LIGHTHILL MJ, 1949, PHILOS MAG, V40, P1179

[10] ON WAVES OF FINITE AMPLITUDE IN DUCTS .1. WAVE FRONTS [J]. QUARTERLY JOURNAL OF MECHANICS AND APPLIED MATHEMATICS, 1952, 5 (03) : 257 - 269