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Home > Reference > Research and information: general > Research methods: general > On Parametric Sensitivity of Reynolds-Averaged Navier-Stokes Sst Turbulence Model: 2D Hypersonic Shock-Wave Boundary Layer Interactions
On Parametric Sensitivity of Reynolds-Averaged Navier-Stokes Sst Turbulence Model: 2D Hypersonic Shock-Wave Boundary Layer Interactions

On Parametric Sensitivity of Reynolds-Averaged Navier-Stokes Sst Turbulence Model: 2D Hypersonic Shock-Wave Boundary Layer Interactions


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About the Book

Examined is sensitivity of separation extent, wall pressure and heating to variation of primary input flow parameters, such as Mach and Reynolds numbers and shock strength, for 2D and Axisymmetric Hypersonic Shock Wave Turbulent Boundary Layer interactions obtained by Navier-Stokes methods using the SST turbulence model. Baseline parametric sensitivity response is provided in part by comparison with vetted experiments, and in part through updated correlations based on free interaction theory concepts. A recent database compilation of hypersonic 2D shock-wave/turbulent boundary layer experiments extensively used in a prior related uncertainty analysis provides the foundation for this updated correlation approach, as well as for more conventional validation. The primary CFD method for this work is DPLR, one of NASA's real-gas aerothermodynamic production RANS codes. Comparisons are also made with CFL3D, one of NASA's mature perfect-gas RANS codes. Deficiencies in predicted separation response of RANS/SST solutions to parametric variations of test conditions are summarized, along with recommendations as to future turbulence approach. Brown, James L. Ames Research Center NAVIER-STOKES EQUATION; TURBULENCE MODELS; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC SHOCK; BOUNDARY LAYER SEPARATION; MACH NUMBER; REYNOLDS NUMBER; AEROTHERMODYNAMICS; WALL PRESSURE; SHOCK WAVE INTERACTION; PRESSURE DISTRIBUTION


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Product Details
  • ISBN-13: 9781719503853
  • Publisher: Createspace Independent Publishing Platform
  • Publisher Imprint: Createspace Independent Publishing Platform
  • Height: 279 mm
  • No of Pages: 66
  • Spine Width: 4 mm
  • Weight: 177 gr
  • ISBN-10: 1719503850
  • Publisher Date: 23 May 2018
  • Binding: Paperback
  • Language: English
  • Returnable: N
  • Sub Title: 2D Hypersonic Shock-Wave Boundary Layer Interactions
  • Width: 216 mm


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On Parametric Sensitivity of Reynolds-Averaged Navier-Stokes Sst Turbulence Model: 2D Hypersonic Shock-Wave Boundary Layer Interactions
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On Parametric Sensitivity of Reynolds-Averaged Navier-Stokes Sst Turbulence Model: 2D Hypersonic Shock-Wave Boundary Layer Interactions
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