This report covers work done in a transonic wind tunnel towards providing data on the influence of the movement of wall-control jacks on the Mach number perturbations along the test section. The data is derived using an existing streamline-curvature program, and in application is reduced to matrices of influence coefficients
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
The techniques used to find aerodynamically straight wall contours in a test section of a transonic ...
The original flexible top and bottom walls of the Transonic Self-Streamlining Wind Tunnel (TSWT), at...
Flexible walled wind tunnels have for some time been used to reduce wall interference effects at the...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
Twenty four test runs of the Transonic Self-Streamlining Wind Tunnel were performed with the flexibl...
Testing in the low speed flexible walled tunnel in an effort to explain the reasons for data discrep...
The first tests conducted in the adaptive-wall test section of the Ames Research Center's 2- by 2-Fo...
A method has been developed for accurately computing the imaginary flow fields outside a flexible wa...
Data for a NACA 0012-64 airfoil at Mach numbers of 0.3, 0.5, and 0.7 with the test section flexible ...
A series of experiments were performed to evaluate the effectiveness of a three-dimensional land and...
Two dimensional airfoil testing in an adaptive wall test-section wind tunnel requires the computatio...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
The first documented wind tunnel employing a flexible walled test section for the purpose of elimina...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
The techniques used to find aerodynamically straight wall contours in a test section of a transonic ...
The original flexible top and bottom walls of the Transonic Self-Streamlining Wind Tunnel (TSWT), at...
Flexible walled wind tunnels have for some time been used to reduce wall interference effects at the...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
Twenty four test runs of the Transonic Self-Streamlining Wind Tunnel were performed with the flexibl...
Testing in the low speed flexible walled tunnel in an effort to explain the reasons for data discrep...
The first tests conducted in the adaptive-wall test section of the Ames Research Center's 2- by 2-Fo...
A method has been developed for accurately computing the imaginary flow fields outside a flexible wa...
Data for a NACA 0012-64 airfoil at Mach numbers of 0.3, 0.5, and 0.7 with the test section flexible ...
A series of experiments were performed to evaluate the effectiveness of a three-dimensional land and...
Two dimensional airfoil testing in an adaptive wall test-section wind tunnel requires the computatio...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
The first documented wind tunnel employing a flexible walled test section for the purpose of elimina...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
The techniques used to find aerodynamically straight wall contours in a test section of a transonic ...
The original flexible top and bottom walls of the Transonic Self-Streamlining Wind Tunnel (TSWT), at...