SAE technical papers on CD-ROM/SAE technical paper series · 1987 · 12 citations · 3 references
EngineeringAerospace EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsAerodynamic TestingComputational AerodynamicsExperimental AerodynamicsJet PropulsionSupersonic AerodynamicsUnsteady AerodynamicsJet ImpingementJetsReynolds NumberReynolds Number EffectsSpacingsUnsteady FlowUnsteady Flow DynamicsUnsteady Lift
<div class="htmlview paragraph">Experiments were performed to simulate jet plume effects associated with VTOL aircraft in takeoff and cruise modes. A water facility was used to investigate the influence of inclination angle and separation distance on the three-dimensional fountain flowfield generated by two impinging jets operating at a jet Reynolds number of 250,000. Substantial differences in the flow features were observed for different spacings between the jets. Plume effects in cruise mode were simulated by a supersonic unheated jet parallel to a wall. Variation of the distance between the wall and the edge of the plume is shown to have a major controlling effect on the supersonic screech instability.</div>
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Advances in high speed jet aeroacoustics
John Seiner · 1984 · 162 citations
Influence of nozzle asymmetry on supersonic jets
Richard W. Wlezien, Valdis Kibens · AIAA Journal · 1988 · 113 citations
Nozzle geometry effects on supersonic jet interaction
Richard W. Wlezien · 1987 · 23 citations