COMPUTATION OF INCOMPRESSIBLE TURBULENT BOUNDARY LAYERS AT LOW REYNOLDS NUMBERS

[1] A FINITE-DIFFERENCE METHOD FOR CALCULATING COMPRESSIBLE LAMINAR AND TURBULENT BOUNDARY LAYERS [J]. JOURNAL OF BASIC ENGINEERING, 1970, 92 (03): : 523 - &

[2] Cebeci T, 1970, AIAA J, V8, P48, DOI [10.2514/3.6079, DOI 10.2514/3.6079]

[3] COLES DE, 1953, 2069 JET PROP LAB RE

[4] COLES DE, 1969, P COMPUTATION TURBUL, V2

[5] COLES DE, 1961, P2417 RAND CORP REPT

[6] SIMPSON RL, 1967, HMT2 STANF U REPT

[7] ON TURBULENT FLOW NEAR A WALL [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (11): : 1007 - &

[1] A FINITE-DIFFERENCE METHOD FOR CALCULATING COMPRESSIBLE LAMINAR AND TURBULENT BOUNDARY LAYERS [J]. JOURNAL OF BASIC ENGINEERING, 1970, 92 (03): : 523 - &

[2] Cebeci T, 1970, AIAA J, V8, P48, DOI [10.2514/3.6079, DOI 10.2514/3.6079]

[3] COLES DE, 1953, 2069 JET PROP LAB RE

[4] COLES DE, 1969, P COMPUTATION TURBUL, V2

[5] COLES DE, 1961, P2417 RAND CORP REPT

[6] SIMPSON RL, 1967, HMT2 STANF U REPT

[7] ON TURBULENT FLOW NEAR A WALL [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (11): : 1007 - &