THE VISCOUS FLOW NEAR A STAGNATION POINT WHEN THE EXTERNAL FLOW HAS UNIFORM VORTICITY

[1] GLAUERT MB, 1957, J AERONAUT SCI, V24, P848

[2] THE LAMINAR BOUNDARY LAYER ON OSCILLATING PLATES AND CYLINDERS [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (01) : 97 - 110

[3] LI TY, 1956, J AERONAUT SCI, V23, P1128

[4] LI TY, 1957, J AERONAUT SCI, V24, P849

[5] LI TY, 1955, J AERONAUT SCI, V22, P651

[6] Lin C. C., 1958, ARCH RATION MECH AN, V1, P391, DOI [10.1007/BF00298016, DOI 10.1007/BF00298016]

[7] ROTT N, 1956, Q APPL MATH, V13, P344

[8] Schlichting H., 1955, BOUNDARY LAYER THEOR

[1] GLAUERT MB, 1957, J AERONAUT SCI, V24, P848

[2] THE LAMINAR BOUNDARY LAYER ON OSCILLATING PLATES AND CYLINDERS [J]. JOURNAL OF FLUID MECHANICS, 1956, 1 (01) : 97 - 110

[3] LI TY, 1956, J AERONAUT SCI, V23, P1128

[4] LI TY, 1957, J AERONAUT SCI, V24, P849

[5] LI TY, 1955, J AERONAUT SCI, V22, P651

[6] Lin C. C., 1958, ARCH RATION MECH AN, V1, P391, DOI [10.1007/BF00298016, DOI 10.1007/BF00298016]

[7] ROTT N, 1956, Q APPL MATH, V13, P344

[8] Schlichting H., 1955, BOUNDARY LAYER THEOR