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Dynamic distortion at the exit of a subsonic diffuser of a mixed compression inlet
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The article was published on 1970-12-01 and is currently open access. It has received 7 citations till now. The article focuses on the topics: Diffuser (thermodynamics) & Distortion.read more
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Journal ArticleDOI
Survey of Validation Data Base for Shockwave Boundary-Layer Interactions in Supersonic Inlets
Awatef Hamed,J. S. Shang +1 more
TL;DR: In this paper, the authors review and assess the data base for shock boundary-layer interaction that is pertinent to the flow prediction in supersonic inlets and identify specific areas related to shock wave/boundary layer interaction bleed, for flow separation control.
Journal ArticleDOI
Investigation of oblique shock/boundary-layer bleed interaction
Awatef Hamed,T. Lehnig +1 more
TL;DR: The detailed flowfield characteristics in an oblique shockwave/laminar boundary-layer interaction with bleed were investigated in this article, where the numerical solution for the flowfield was obtained for the strong conservation-law form of the two-dimensional compressible Navier-Stokes equations using an implicit scheme.
Shock-Wave/Boundary-Layer Interactions with Bleed Part 2: Effect of Slot Location
TL;DR: In this paper, the effect of bleed configuration in the interaction region of an oblique shock wave and a turbulent boundary layer was investigated using numerical simulations and the numerical solution was obtained for the compressible Navier-Stokes and A>£ equations throughout the interaction zone and inside the slanted and normal bleed slots.
Journal ArticleDOI
Effect of bleed configuration on shock/laminar boundary-layer interactions
Awatef Hamed,T. Lehnig +1 more
TL;DR: In this article, the flowfield characteristics are simulated numerically in an oblique shock wave/laminar boundary-layer interaction for three different bleed configurations for different bleed locations and the detailed flow characteristics in the interaction zone and inside the bleed slot are compared for the three cases.
Proceedings ArticleDOI
The effect of bleed configuration on shock/boundary layer interactions
Awatef Hamed,T. Lehnig +1 more
TL;DR: In this paper, the flow field characteristics were simulated numerically in an oblique shock wave/laminar boundary layer interaction for three different bleed configurations, and detailed flow characteristics in the interaction zone and inside the bleed slot were compared for the three cases.
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Boundary-layer analysis of subsonic inlet diffuser geometries for engines nacelles
J. A. Albers,E. J. Felderman +1 more