AN EXTENSION OF THE THEORY OF THE ONE-DIMENSIONAL SHOCK-WAVE STRUCTURE

[1] BECKER R, 1929, NACA TM505

[2] BETHE HA, X117 BALL RES LAB RE

[3] CHANG CSW, 1948, APLJHU CM503 U MICH

[4] EGGERS AJ, 1949, NACA TN1861

[5] KEENAN JH, 1945, THERMODYNAMIC PROPER

[6] Lamb H, 1945, HYDRODYNAMICS, V6th

[7] MEYERHOFF L, 1949, PIBAL150

[8] MEYERHOFF L, 1949, THESIS POLYTECHNIC I

[9] 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 - &

[10] PRANDTL L, 1906, Z GESAMTE TURBINEN W, V3, P241

[1] BECKER R, 1929, NACA TM505

[2] BETHE HA, X117 BALL RES LAB RE

[3] CHANG CSW, 1948, APLJHU CM503 U MICH

[4] EGGERS AJ, 1949, NACA TN1861

[5] KEENAN JH, 1945, THERMODYNAMIC PROPER

[6] Lamb H, 1945, HYDRODYNAMICS, V6th

[7] MEYERHOFF L, 1949, PIBAL150

[8] MEYERHOFF L, 1949, THESIS POLYTECHNIC I

[9] 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 - &

[10] PRANDTL L, 1906, Z GESAMTE TURBINEN W, V3, P241