An integral method for calculating the nonsimilar steady two-dimensional boundary-layer development on both upstream and downstream moving walls has been developed. Separation from moving walls is briefly reviewed and a separation criterion for the technique is developed that conforms with some accepted ideas on boundary-layer separation. The integral-momentum and integral-energy boundary-layer equations have been integrated simultaneously by using the shape factor relationships derived from moving-wall similarity solutions. The results are found to compare favorably with an exact solution and an approximate solution. The stability of the boundary-layer development calculations is also examined."June 1975."Includes bibliographic references ...
A shear-work integral method is developed for calculating compressible turbulent boundary layers on ...
The results of experimental study on a boundary layer separation control are given in the paper. The...
A general integral form oj the ibundary-layer equation i8 dericed from the Prandtl partial-di~erenti...
Similarity solutions for moving wall, two dimensional, incompressible boundary layer equations are r...
The nonsimilar moving wall stagnation point solution derived by Rott has been redefined so as to sho...
A numerical evaluation of this solution carried out the data obtained in a curving nonrotating duct ...
In computational fluid dynamics, wall function boundary conditions are essential for the treatment o...
This paper presents a mathematical discussion of the laminar boundary layer, which was developed wit...
A single analytical expression is proposed to describe the velocity distribution in a two-dimensiona...
This paper presents a mathematical discussion of the laminar boundary layer, which was developed wit...
Includes bibliographical referencesA new coordinate and variable transformation for the two-dimensio...
A momentum integral method is developed to predict the growth of three dimensional turbulent bounda...
A single analytical expression is derived for the entire (0 <or = y <infinity) velocity distribution...
The boundary-layer flow over a moving continuous solid surface is important in several engineering p...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
A shear-work integral method is developed for calculating compressible turbulent boundary layers on ...
The results of experimental study on a boundary layer separation control are given in the paper. The...
A general integral form oj the ibundary-layer equation i8 dericed from the Prandtl partial-di~erenti...
Similarity solutions for moving wall, two dimensional, incompressible boundary layer equations are r...
The nonsimilar moving wall stagnation point solution derived by Rott has been redefined so as to sho...
A numerical evaluation of this solution carried out the data obtained in a curving nonrotating duct ...
In computational fluid dynamics, wall function boundary conditions are essential for the treatment o...
This paper presents a mathematical discussion of the laminar boundary layer, which was developed wit...
A single analytical expression is proposed to describe the velocity distribution in a two-dimensiona...
This paper presents a mathematical discussion of the laminar boundary layer, which was developed wit...
Includes bibliographical referencesA new coordinate and variable transformation for the two-dimensio...
A momentum integral method is developed to predict the growth of three dimensional turbulent bounda...
A single analytical expression is derived for the entire (0 <or = y <infinity) velocity distribution...
The boundary-layer flow over a moving continuous solid surface is important in several engineering p...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
A shear-work integral method is developed for calculating compressible turbulent boundary layers on ...
The results of experimental study on a boundary layer separation control are given in the paper. The...
A general integral form oj the ibundary-layer equation i8 dericed from the Prandtl partial-di~erenti...