Add to ORKGA total of 142 shadowgraph photographs were taken on 43 different plumes that were distributed over the six nozzle configurations using the 9.5 inch diameter collimated light beam of the shadowgraph setup. Aerodynamic flow conditions of the shadowgraph test points, the location and identification of each of the photographs, and copies of the pictures are presented
The paper reports flow visualizations of a free slot jet of air, obtained with the shadowgraph techn...
The desire to reduce or eliminate the operational restrictions of supersonic aircraft over populated...
A wind tunnel test and a computational study were conducted to investigate the complex interactions ...
"Prepared [at GE Aircraft Engine Business Group] for Lewis Research Center under contract NAS3-22514...
The plume produced by a cluster of two high area-ratio thrust optimized parabolic contour nozzles is...
Shadowgraph photography techniques in transonic wind tunnel tests are described. The system was used...
"November 1984"--Cover.STAR category 71.Distributed to depository libraries in microfiche."General E...
textThe plume produced by a cluster of two large area-ratio thrust optimized parabolic contour nozzl...
Design and implementation of a test bench for an aerospike nozzle allowing the visualization of comp...
Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...
A novel shadowgraph flow visualisation technique has been developed and used to visualise key region...
Shadowgraph techniques were applied to the cold flow ejector facility at the Propulsion Research Cen...
Seven single stream model nozzles were tested in the Anechoic Free-Jet Acoustic Test Facility to eva...
A simple and robust retroreflective shadowgraph technique is presented for the visualization of refr...
Pressure distribution data were obtained on several sharp leading edge wings, conical bodies, and bo...
The paper reports flow visualizations of a free slot jet of air, obtained with the shadowgraph techn...
The desire to reduce or eliminate the operational restrictions of supersonic aircraft over populated...
A wind tunnel test and a computational study were conducted to investigate the complex interactions ...
"Prepared [at GE Aircraft Engine Business Group] for Lewis Research Center under contract NAS3-22514...
The plume produced by a cluster of two high area-ratio thrust optimized parabolic contour nozzles is...
Shadowgraph photography techniques in transonic wind tunnel tests are described. The system was used...
"November 1984"--Cover.STAR category 71.Distributed to depository libraries in microfiche."General E...
textThe plume produced by a cluster of two large area-ratio thrust optimized parabolic contour nozzl...
Design and implementation of a test bench for an aerospike nozzle allowing the visualization of comp...
Parameters which contribute to supersonic jet shock noise were investigated for the purpose of deter...
A novel shadowgraph flow visualisation technique has been developed and used to visualise key region...
Shadowgraph techniques were applied to the cold flow ejector facility at the Propulsion Research Cen...
Seven single stream model nozzles were tested in the Anechoic Free-Jet Acoustic Test Facility to eva...
A simple and robust retroreflective shadowgraph technique is presented for the visualization of refr...
Pressure distribution data were obtained on several sharp leading edge wings, conical bodies, and bo...
The paper reports flow visualizations of a free slot jet of air, obtained with the shadowgraph techn...
The desire to reduce or eliminate the operational restrictions of supersonic aircraft over populated...
A wind tunnel test and a computational study were conducted to investigate the complex interactions ...