Add to ORKGThis experimental inrestigaiion was conducted pri-marily for the purpose OJobtaining a method of corre&”ng to free air conditions the results of airfm”lforce tests in ~our open m“nd tunnel jets of different shapw Tests were also made to determine whether the jet boundaries had any appreeiabk eject on the gn”khingmoment8 of a complete airplane model. The inreetigation was con-cluded in the Atmospheric IWind Tunnel of the.Lmgley Memorial Aeronautical Laboratory. 17te method of obtaining the airfoil corrections utilized the results of force fest~made in eachjet on three similar monoplan
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
This report outlines the development of a general theory for the calculation of the effect of the bo...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
This experimental investigation was conducted primarily for the purpose of obtaining a method of cor...
Prandtl's suggested use of a doubly infinite arrangement of airfoil images in the theoretical determ...
The interference of the wind-tunnel boundaries on the downwash behind an airfoil has been experiment...
Prandtl's suggested use of a doubly infinite arrangement of airfoil images in the theoretical determ...
The interference of the wind-tunnel boundaries on the downwash behind an airfoil has been experiment...
The presence of nearby boundaries in a wind tunnel can lead to aerodynamic measurements on a model i...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
Jet boundary corrections for partly open and partly closed elliptical wind tunnels for the cases of ...
A detailed method for determining the jet-boundary corrections for reflection-plane models in rectan...
Accurate measurements of rotorcraft performance as measured in a wind tunnel are strongly influenced...
The results of an experimental investigation on the boundary-correction factor are presented in this...
Sophisticated methods have become available for computing wind tunnel boundary corrections; this has...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
This report outlines the development of a general theory for the calculation of the effect of the bo...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
This experimental investigation was conducted primarily for the purpose of obtaining a method of cor...
Prandtl's suggested use of a doubly infinite arrangement of airfoil images in the theoretical determ...
The interference of the wind-tunnel boundaries on the downwash behind an airfoil has been experiment...
Prandtl's suggested use of a doubly infinite arrangement of airfoil images in the theoretical determ...
The interference of the wind-tunnel boundaries on the downwash behind an airfoil has been experiment...
The presence of nearby boundaries in a wind tunnel can lead to aerodynamic measurements on a model i...
The theory of wind tunnel boundary influence on the downwash from a wing has been extended to provid...
Jet boundary corrections for partly open and partly closed elliptical wind tunnels for the cases of ...
A detailed method for determining the jet-boundary corrections for reflection-plane models in rectan...
Accurate measurements of rotorcraft performance as measured in a wind tunnel are strongly influenced...
The results of an experimental investigation on the boundary-correction factor are presented in this...
Sophisticated methods have become available for computing wind tunnel boundary corrections; this has...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
This report outlines the development of a general theory for the calculation of the effect of the bo...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...