Direct simulation of hypersonic flows over blunt wedges
Author:
Affiliation:
1. Old Dominion University Research Foundation, Norfolk, Virginia
2. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11
Reference15 articles.
1. Laminar convective heat-transfer rates on a hemisphere cylinder in rarefied hypersonic flow
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1. Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows;Journal of Applied Mathematics and Mechanics;2016
2. Analytical prediction of heat transfer and skin friction in 3D transitional hypersonic flows over blunt bodies;AIP Conference Proceedings;2014
3. Chapter 17: Analytical Method of Solving Thin Viscous Shock Layer Equations at Low Reynolds Numbers;Hypersonic Aerodynamics and Heat Transfer;2013
4. Aerothermodynamic Analysis of a Reentry Brazilian Satellite;Brazilian Journal of Physics;2012-10-06
5. The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow;Journal of Applied Mathematics and Mechanics;2012-01
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