Add to ORKGThe new wall pressure measurement system and the TWICS wall correction system for the 14x22-Ft subsonic tunnel are described. Results from a recent semispan test and a full-span test are presented. Comparison with existing classical methods of correction is shown. A modification of the TWICS code to treat the effect due to a deflected wake from a high-lift wing is also discussed. The current implementation of TWICS for the 14x22-Ft tunnel is shown to be an improvement over existing methods
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
Airfoil characteristics measured in a wind tunnel typically differ from those obtained in free air d...
Calibrations were obtained in the Langley 6 by 28-inch transonic tunnel with newly installed control...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
A Fortran subroutine CMWALL is described, which is an implementation of the collective information f...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
The test section walls of the NASA Langley Research Center 14- by 22-Foot Subsonic Tunnel are known ...
An off-line version of the Wall Interference Correction System (WICS) has been implemented for the N...
An off-line version of the Wall Interference Correction System (WICS) has been implemented for the "...
The purpose of this research was to demonstrate the viability of a method, due to Professor W. R. Se...
The results of a new subsonic calibration of the Langley 7 by 10 foot high speed tunnel with the tes...
This paper describes the new wall pressure measurement system and data-quality monitoring software i...
The Modern Design of Experiments (MDOE) has been applied to wind tunnel testing at NASA Langley Rese...
Data from the test of a large semispan model was used to perform a direct validation of a wall inter...
Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical r...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
Airfoil characteristics measured in a wind tunnel typically differ from those obtained in free air d...
Calibrations were obtained in the Langley 6 by 28-inch transonic tunnel with newly installed control...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
A Fortran subroutine CMWALL is described, which is an implementation of the collective information f...
The Wall Interference Correction System (WICS) is operational at the National Transonic Facility (NT...
The test section walls of the NASA Langley Research Center 14- by 22-Foot Subsonic Tunnel are known ...
An off-line version of the Wall Interference Correction System (WICS) has been implemented for the N...
An off-line version of the Wall Interference Correction System (WICS) has been implemented for the "...
The purpose of this research was to demonstrate the viability of a method, due to Professor W. R. Se...
The results of a new subsonic calibration of the Langley 7 by 10 foot high speed tunnel with the tes...
This paper describes the new wall pressure measurement system and data-quality monitoring software i...
The Modern Design of Experiments (MDOE) has been applied to wind tunnel testing at NASA Langley Rese...
Data from the test of a large semispan model was used to perform a direct validation of a wall inter...
Wind tunnel wall interference assessment and correction (WIAC) concepts, applications, and typical r...
From the time that wind tunnel wall interference was recognized to be significant, researchers have ...
Airfoil characteristics measured in a wind tunnel typically differ from those obtained in free air d...
Calibrations were obtained in the Langley 6 by 28-inch transonic tunnel with newly installed control...