Calculation of three dimensional laminar boundary layer in a noncompressible liquid by method of integral relationships
Abstract
Integral equations are derived for these boundary layers, and the finite difference theory is included. Friction coefficients are given for several velocity distributions on the sliding wing wall.
 Publication:

NASA STI/Recon Technical Report N
 Pub Date:
 January 1975
 Bibcode:
 1975STIN...7522646B
 Keywords:

 Incompressible Fluids;
 Integral Equations;
 Laminar Boundary Layer;
 Three Dimensional Boundary Layer;
 Coefficient Of Friction;
 Equations Of Motion;
 Finite Difference Theory;
 Gas Dynamics;
 Fluid Mechanics and Heat Transfer