Add to ORKGThe principal sources of flow unsteadiness in the circuit of a transonic wind tunnel are presented. Care must be taken to avoid flow separations, acoustic resonances and large scale turbulence. Some problems discussed are the elimination of diffuser separations, the aerodynamic design of coolers and the unsteadiness generated in ventilated working sections
The results of detailed parametric experiments are presented for the near-wall flow field of a longi...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
Comprehensive aerodynamic data on an airfoil section were obtained through a wide range of angles of...
A compilation of lectures presented at various Universities over a span of several years is discusse...
During the past years, there was an extensive program under way at the Langley Research Center to up...
Pressure fluctuations have been measured over the course of several tests in the National Transonic ...
The mean velocity profiles in both the horizontal and vertical planes of symmetry at specific locati...
The measurement of wind tunnel background pressure fluctuations in a Ludwig Tube is discussed. The m...
Report presents an approximate subsonic theory for the solid-blockage interference in circular wind ...
Unsteady Pressure Measurements In The NAL 1.2m Trisonic Wind Tunnel Indicated That Levels Of Test Se...
The principles of flow generation in ventilated-wall transonic test-section are briefly reviewed. ...
Problems in modeling the complex interacting flow fields in the transonic speed regime are reviewed....
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
State-of-the art instrumentation and procedures for calibrating transonic (0.6 less than M less than...
Transfer of an existing continous circuit supersonic wind tunnel to Langley and its operation there ...
The results of detailed parametric experiments are presented for the near-wall flow field of a longi...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
Comprehensive aerodynamic data on an airfoil section were obtained through a wide range of angles of...
A compilation of lectures presented at various Universities over a span of several years is discusse...
During the past years, there was an extensive program under way at the Langley Research Center to up...
Pressure fluctuations have been measured over the course of several tests in the National Transonic ...
The mean velocity profiles in both the horizontal and vertical planes of symmetry at specific locati...
The measurement of wind tunnel background pressure fluctuations in a Ludwig Tube is discussed. The m...
Report presents an approximate subsonic theory for the solid-blockage interference in circular wind ...
Unsteady Pressure Measurements In The NAL 1.2m Trisonic Wind Tunnel Indicated That Levels Of Test Se...
The principles of flow generation in ventilated-wall transonic test-section are briefly reviewed. ...
Problems in modeling the complex interacting flow fields in the transonic speed regime are reviewed....
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
State-of-the art instrumentation and procedures for calibrating transonic (0.6 less than M less than...
Transfer of an existing continous circuit supersonic wind tunnel to Langley and its operation there ...
The results of detailed parametric experiments are presented for the near-wall flow field of a longi...
An airfoil design program and a boundary layer analysis were developed. Boundary conditions were der...
Comprehensive aerodynamic data on an airfoil section were obtained through a wide range of angles of...