A PHILOSOPHY FOR IMPROVED ROCKET NOZZLE DESIGN

[1] CHAPMAN DR, 1950, NACA TN2137

[2] CLIPPINGER RF, 1951, BRL794 AB PROV GROUN

[3] Courant R., 1948, SUPERSONIC FLOW SHOC

[4] DEHALLER P, 1945, SULZER TECHNICAL REV, V1

[5] FALKOVICH SV, 1949, NACA TN1212

[6] FERRI A, 1949, ELEMENTS AERODYNAMIC, pCH10

[7] FERRI A, 1946, NACA TN1135

[8] GUDERLEY G, 1955, Z FLUGWISSENSCHAFTEN, V13, pN9

[9] HOOKER SC, 1931, ARC REM1429

[10] ISENBERG JS, 1947, MONOGRAPH TECHNICAL, V2

[1] CHAPMAN DR, 1950, NACA TN2137

[2] CLIPPINGER RF, 1951, BRL794 AB PROV GROUN

[3] Courant R., 1948, SUPERSONIC FLOW SHOC

[4] DEHALLER P, 1945, SULZER TECHNICAL REV, V1

[5] FALKOVICH SV, 1949, NACA TN1212

[6] FERRI A, 1949, ELEMENTS AERODYNAMIC, pCH10

[7] FERRI A, 1946, NACA TN1135

[8] GUDERLEY G, 1955, Z FLUGWISSENSCHAFTEN, V13, pN9

[9] HOOKER SC, 1931, ARC REM1429

[10] ISENBERG JS, 1947, MONOGRAPH TECHNICAL, V2