A Wall Signature method originally developed by Hackett has been selected to be adapted for the Ames 12-ft Wind Tunnel WIAC system in the project. This method uses limited measurements of the static pressure at the wall, in conjunction with the solid wall boundary condition, to determine the strength and distribution of singularities representing the test article. The singularities are used in turn for estimating wall interference at the model location. The development and implementation of a working prototype will be completed, delivered and documented with a software manual. The WIAC code will be validated by conducting numerically simulated experiments rather than actual wind tunnel experiments. The simulations will be used to generate b...
The main objective of this work is the development and application of a wall pressure-signature meth...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
A Wall Signature method originally developed by Hackett has been selected to be adapted for the Ames...
A wall signature method has been selected to be adapted for the Ames 12-ft Wind Tunnel WIAC system. ...
A Wall Signature method, the Hackett method, has been selected to be adapted for the 12-ft Wind Tunn...
The Hackett method (a Wall Pressure Signature Method) was selected to be adapted for the 12 ft Wind ...
Development of complex air vehicle configurations is placing increasing demands on wind tunnel testi...
Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical r...
Technical information focused upon emerging wall interference assessment/correction (WIAC) technique...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
The new check standard model of the NASA Ames 11-ft Transonic Wind Tunnel was chosen for a future va...
A wind-tunnel interference assessment method applicable to test sections with discrete finite-length...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
A brief review is made of the methods currently available for assessing and correcting the data for ...
The main objective of this work is the development and application of a wall pressure-signature meth...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
A Wall Signature method originally developed by Hackett has been selected to be adapted for the Ames...
A wall signature method has been selected to be adapted for the Ames 12-ft Wind Tunnel WIAC system. ...
A Wall Signature method, the Hackett method, has been selected to be adapted for the 12-ft Wind Tunn...
The Hackett method (a Wall Pressure Signature Method) was selected to be adapted for the 12 ft Wind ...
Development of complex air vehicle configurations is placing increasing demands on wind tunnel testi...
Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical r...
Technical information focused upon emerging wall interference assessment/correction (WIAC) technique...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
The new check standard model of the NASA Ames 11-ft Transonic Wind Tunnel was chosen for a future va...
A wind-tunnel interference assessment method applicable to test sections with discrete finite-length...
A method for analyzing wall interference is described which avoids the assumption of linear superpos...
A brief review is made of the methods currently available for assessing and correcting the data for ...
The main objective of this work is the development and application of a wall pressure-signature meth...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...