VORTICITY AND KUTTA CONDITION FOR UNSTEADY MULTIENERGY FLOWS

[1] Giesing J. P., 1968, J AIRCRAFT, V5, P135, DOI DOI 10.2514/3.43920

[2] GIESING JP, 1968, T ASME D, V90, P387

[3] MILNETHOMSON LM, 1961, THERETICAL HYDRODYNA

[4] DIFFRACTION OF A WEAK SHOCK WITH VORTEX GENERATION [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (01) : 111 - 128

[5] SOME RECENT DEVELOPMENTS IN AIRFOIL THEORY [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (05): : 490 - 499

[6] VANDEVOOREN AI, 1964, ARCHIWUM MECHANIKI S, V3, P709

[7] von Karman T, 1938, J AERONAUT SCI, V5, P379, DOI [DOI 10.2514/8.674, 10.2514/8.674]

[1] Giesing J. P., 1968, J AIRCRAFT, V5, P135, DOI DOI 10.2514/3.43920

[2] GIESING JP, 1968, T ASME D, V90, P387

[3] MILNETHOMSON LM, 1961, THERETICAL HYDRODYNA

[4] DIFFRACTION OF A WEAK SHOCK WITH VORTEX GENERATION [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (01) : 111 - 128

[5] SOME RECENT DEVELOPMENTS IN AIRFOIL THEORY [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (05): : 490 - 499

[6] VANDEVOOREN AI, 1964, ARCHIWUM MECHANIKI S, V3, P709

[7] von Karman T, 1938, J AERONAUT SCI, V5, P379, DOI [DOI 10.2514/8.674, 10.2514/8.674]