TURBULENT BOUNDARY LAYER IN COMPRESSIBLE FLUIDS

[1] Ackerman G., 1942, FORSCH GEB INGENIEUR, V13, P226, DOI [10.1007/BF02585341, DOI 10.1007/BF02585341]

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

[3] CROCCO L, 1931, RENDICONTI R ACAD LI, V14, P490

[4] FERRARI C, 1950, Q APPLIED MATH, V8

[5] FRANKL F, 1943, NACA TM1053

[6] Karman T.V., 1934, J AERO SCI, V1, P1, DOI DOI 10.2514/8.5

[7] SCHUBAUER GB, 1950, NACA TN2133

[8] SPIVACK HM, 1950, AL1052 N AM AV REP

[9] TRIBUS M, 1942, NACA ARR OCT

[10] VANDRIEST ER, 1950, AL1044 N AM AV REP

[1] Ackerman G., 1942, FORSCH GEB INGENIEUR, V13, P226, DOI [10.1007/BF02585341, DOI 10.1007/BF02585341]

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

[3] CROCCO L, 1931, RENDICONTI R ACAD LI, V14, P490

[4] FERRARI C, 1950, Q APPLIED MATH, V8

[5] FRANKL F, 1943, NACA TM1053

[6] Karman T.V., 1934, J AERO SCI, V1, P1, DOI DOI 10.2514/8.5

[7] SCHUBAUER GB, 1950, NACA TN2133

[8] SPIVACK HM, 1950, AL1052 N AM AV REP

[9] TRIBUS M, 1942, NACA ARR OCT

[10] VANDRIEST ER, 1950, AL1044 N AM AV REP