SOME FEATURES OF BOUNDARY LAYERS AND TRANSITION TO TURBULENT FLOW

[1] ACKERET J, 1947, NACA TM1113

[2] ALLEN HJ, 1951, NACA REP, V1048

[3] ALTMAN JM, 1951, NACA TN2500

[4] ASHKENAS HL, 1955, NACA TN3383

[5] BOGDONOFF SM, 1955, SOME EXPT STUDIES SE

[6] BRASLOW AL, 1951, NACA REP, V1025

[7] Gas flow with laminary barriers along a plate [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1935, 15 : 23 - 25

[8] MEASUREMENTS OF TURBULENT SKIN FRICTION ON CYLINDERS IN AXIAL FLOW AT SUBSONIC AND SUPERSONIC VELOCITIES [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07): : 441 - 448

[9] CHARTERS AC, 1943, NACA TN891

[10] CLAUSER FH, 1954, J AERONAUT SCI, V2, P91

[1] ACKERET J, 1947, NACA TM1113

[2] ALLEN HJ, 1951, NACA REP, V1048

[3] ALTMAN JM, 1951, NACA TN2500

[4] ASHKENAS HL, 1955, NACA TN3383

[5] BOGDONOFF SM, 1955, SOME EXPT STUDIES SE

[6] BRASLOW AL, 1951, NACA REP, V1025

[7] Gas flow with laminary barriers along a plate [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1935, 15 : 23 - 25

[8] MEASUREMENTS OF TURBULENT SKIN FRICTION ON CYLINDERS IN AXIAL FLOW AT SUBSONIC AND SUPERSONIC VELOCITIES [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (07): : 441 - 448

[9] CHARTERS AC, 1943, NACA TN891

[10] CLAUSER FH, 1954, J AERONAUT SCI, V2, P91