Add to ORKGData for a NACA 0012-64 airfoil at Mach numbers of 0.3, 0.5, and 0.7 with the test section flexible walls set in the "straight" position are presented because they may prove useful in the development of wind tunnel correction techniques
A method has been developed for accurately computing the imaginary flow fields outside a flexible wa...
Wind tunnels can now simulate flows over airfoils at high Reynolds numbers and high subsonic speeds....
Tests were conducted in the two-dimensional test section of the Langley 0.3-m Transonic Cryogenic Tu...
Twenty four test runs of the Transonic Self-Streamlining Wind Tunnel were performed with the flexibl...
Further flexible wall technique validation in two dimensional testing was carried out with the trans...
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...
Testing in the low speed flexible walled tunnel in an effort to explain the reasons for data discrep...
A wind-tunnel investigation of a CAST 10-2/DOA 2 airfoil model has been conducted in the adaptive-wa...
Two wind tunnel investigations were conducted to assess two different wall interference alleviation/...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
The first tests conducted in the adaptive-wall test section of the Ames Research Center's 2- by 2-Fo...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
Comprehensive aerodynamic data on an airfoil section were obtained through a wide range of angles of...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
A method has been developed for accurately computing the imaginary flow fields outside a flexible wa...
Wind tunnels can now simulate flows over airfoils at high Reynolds numbers and high subsonic speeds....
Tests were conducted in the two-dimensional test section of the Langley 0.3-m Transonic Cryogenic Tu...
Twenty four test runs of the Transonic Self-Streamlining Wind Tunnel were performed with the flexibl...
Further flexible wall technique validation in two dimensional testing was carried out with the trans...
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...
Testing in the low speed flexible walled tunnel in an effort to explain the reasons for data discrep...
A wind-tunnel investigation of a CAST 10-2/DOA 2 airfoil model has been conducted in the adaptive-wa...
Two wind tunnel investigations were conducted to assess two different wall interference alleviation/...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
The first tests conducted in the adaptive-wall test section of the Ames Research Center's 2- by 2-Fo...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
Comprehensive aerodynamic data on an airfoil section were obtained through a wide range of angles of...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
A method has been developed for accurately computing the imaginary flow fields outside a flexible wa...
Wind tunnels can now simulate flows over airfoils at high Reynolds numbers and high subsonic speeds....
Tests were conducted in the two-dimensional test section of the Langley 0.3-m Transonic Cryogenic Tu...