Add to ORKGA transonic similarity rule which accounts for the effects of attached sidewall boundary layers is presented and evaluated by comparison with the characteristics of airfoils tested in a two dimensional transonic tunnel with different sidewall boundary layer thicknesses. The rule appears valid provided the sidewall boundary layer both remains attached in the vicinity of the model and occupies a small enough fraction of the tunnel width to preserve sufficient two dimensionality in the tunnel
A method for assessing the wall interference in transonic two dimensional wind tunnel test was devel...
The laminar boundary layer on a 10 degree cone in a transonic wind tunnel was studied. The inviscid ...
A discussion of the flow field measurements obtained in the vertical plane at several stations along...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
Correction of airfoil data for sidewall boundary-layer effects requires a knowledge of the boundary-...
The effect of sidewall boundary layers in airfoil testing in two-dimensional wind tunnels is investi...
Tables for correcting airfoil data taken in the Langley 0.3-meter Transonic Cryogenic Tunnel for the...
A numerical investigation of the interaction between a wind tunnel sidewall boundary layer and a thi...
The Langley 0.3 Meter Transonic Cryogenic Tunnel has provision for boundary removal from the sidewal...
A simplified fourwall interference assessment method has been described, and a computer program deve...
A method for assessing the wall interference in transonic two-dimensional wind tunnel tests includin...
A synthesis of current trends in the reduction and computation of wall effects is presented. Some of...
An analytical procedure is discussed for designing wall shapes for streamlined, nonporous, two-dimen...
This report presents the corrected aerodynamic data for A NASA SC(2)-0714 airfoil tested in the Lang...
A theoretical examination of the slotted-wall flow field is conducted to determine the appropriate w...
A method for assessing the wall interference in transonic two dimensional wind tunnel test was devel...
The laminar boundary layer on a 10 degree cone in a transonic wind tunnel was studied. The inviscid ...
A discussion of the flow field measurements obtained in the vertical plane at several stations along...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
Correction of airfoil data for sidewall boundary-layer effects requires a knowledge of the boundary-...
The effect of sidewall boundary layers in airfoil testing in two-dimensional wind tunnels is investi...
Tables for correcting airfoil data taken in the Langley 0.3-meter Transonic Cryogenic Tunnel for the...
A numerical investigation of the interaction between a wind tunnel sidewall boundary layer and a thi...
The Langley 0.3 Meter Transonic Cryogenic Tunnel has provision for boundary removal from the sidewal...
A simplified fourwall interference assessment method has been described, and a computer program deve...
A method for assessing the wall interference in transonic two-dimensional wind tunnel tests includin...
A synthesis of current trends in the reduction and computation of wall effects is presented. Some of...
An analytical procedure is discussed for designing wall shapes for streamlined, nonporous, two-dimen...
This report presents the corrected aerodynamic data for A NASA SC(2)-0714 airfoil tested in the Lang...
A theoretical examination of the slotted-wall flow field is conducted to determine the appropriate w...
A method for assessing the wall interference in transonic two dimensional wind tunnel test was devel...
The laminar boundary layer on a 10 degree cone in a transonic wind tunnel was studied. The inviscid ...
A discussion of the flow field measurements obtained in the vertical plane at several stations along...