Four methods of predicting the integral and friction parameters for a turbulent boundary layer over a moving ground plane were evaluated by using test information obtained in 76.2- by 50.8-centimeter tunnel. The tunnel was operated in the open sidewall configuration. These methods are (1) relative integral parameter method, (2) modified power law method, (3) relative power law method, and (4) modified law of the wall method. The modified law of the wall method predicts a more rapid decrease in skin friction with an increase in the ratio of belt velocity to free steam velocity than do methods (1) and (3)
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
Methods of predicting integral parameters and skin-friction coefficients of turbulent boundary layer...
The equations presented can be used to predict the shape factor and the ratio of the momentum thickn...
An analysis has been made of a considerable amount of data for turbulent boundary layers along wings...
Among the information presented are included displacement, momentum, and kinetic energy thicknesses,...
Theoretical studies are made of three dimensional turbulent boundary layer behavior on fixed grounds...
Initial measurements of the changes in local skin friction, velocity profile shape, and turbulence s...
Wind tunnel study of scale model automobile ground plane boundary layer using moving-belt ground pla...
An analysis is presented of the reliability of various generally accepted empirical expressions for ...
A theory for the description of turbulent boundary layer flows over surfaces with a sudden change in...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...
Methods of predicting integral parameters and skin friction coefficients of turbulent boundary layer...
Methods of predicting integral parameters and skin-friction coefficients of turbulent boundary layer...
The equations presented can be used to predict the shape factor and the ratio of the momentum thickn...
An analysis has been made of a considerable amount of data for turbulent boundary layers along wings...
Among the information presented are included displacement, momentum, and kinetic energy thicknesses,...
Theoretical studies are made of three dimensional turbulent boundary layer behavior on fixed grounds...
Initial measurements of the changes in local skin friction, velocity profile shape, and turbulence s...
Wind tunnel study of scale model automobile ground plane boundary layer using moving-belt ground pla...
An analysis is presented of the reliability of various generally accepted empirical expressions for ...
A theory for the description of turbulent boundary layer flows over surfaces with a sudden change in...
An analysis of the incompressible turbulent boundary layer, developing under the combined effects of...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
Computer program predicts growth of boundary layers along any surface where air is flowing. Two inte...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...
A simple method i s presented t o determine the skin13; friction from the measured two dimensional t...