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Numerical Simulation Of Supersonic Flow Using A New Analytical Bleed Boundary Condition by G. J. Harloff
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1NASA Technical Reports Server (NTRS) 19950026787: Numerical Simulation Of Supersonic Flow Using A New Analytical Bleed Boundary Condition
By NASA Technical Reports Server (NTRS)
A new analytical bleed boundary condition is used to compute flowfields for a strong oblique shock wave/boundary layer interaction with a baseline and three bleed rates at a freestream Mach number of 2.47 with an 8 deg shock generator. The computational results are compared to experimental Pitot pressure profiles and wall static pressures through the interaction region. An algebraic turbulence model is employed for the bleed and baseline cases, and a one equation model is also used for the baseline case where the boundary layer is separated.
“NASA Technical Reports Server (NTRS) 19950026787: Numerical Simulation Of Supersonic Flow Using A New Analytical Bleed Boundary Condition” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19950026787: Numerical Simulation Of Supersonic Flow Using A New Analytical Bleed Boundary Condition
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19950026787: Numerical Simulation Of Supersonic Flow Using A New Analytical Bleed Boundary Condition” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - BOUNDARY LAYER CONTROL - COMPUTATIONAL FLUID DYNAMICS - FLOW DISTRIBUTION - OBLIQUE SHOCK WAVES - SHOCK WAVE INTERACTION - SUPERSONIC BOUNDARY LAYERS - SUPERSONIC FLOW - SUPERSONIC INLETS - BOUNDARY LAYER SEPARATION - MACH NUMBER - PRESSURE DISTRIBUTION - SUCTION - TURBULENCE MODELS - Harloff, G. J. - Smith, G. E.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19950026787
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 39.37 Mbs, the file-s for this book were downloaded 57 times, the file-s went public at Mon Oct 10 2016.
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