An attempt has been made to develop a method for predicting the development of turbulent boundary layers in adverse pressure gradient. Simple calculation procedure is presented by incorp-orating a deceleration rate parameter into boundary layer equations. The compressibility effect of the flow is considered° by adopting the Mach number in the momentum and skin friction relations. The predictions of the boundary layers are in good agreement with available experimental results,which validates the calculational technique.
EL-KERSH, A. (1985). ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT. International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), 39-60. doi: 10.21608/asat.1985.26465
MLA
A. M. EL-KERSH. "ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT". International Conference on Aerospace Sciences and Aviation Technology, 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, 1985, 39-60. doi: 10.21608/asat.1985.26465
HARVARD
EL-KERSH, A. (1985). 'ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT', International Conference on Aerospace Sciences and Aviation Technology, 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO), pp. 39-60. doi: 10.21608/asat.1985.26465
VANCOUVER
EL-KERSH, A. ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT. International Conference on Aerospace Sciences and Aviation Technology, 1985; 1(A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO): 39-60. doi: 10.21608/asat.1985.26465
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