Adaptive finite element analysis of hypersonic laminar flows for aerothermal load predictions
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia 23508
2. University of Virginia, Charlottesville, Virginia 22903
3. NASA Langley Research Center, Hampton, Virginia 23665
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/10.2514/3.265
Reference24 articles.
1. A new finite element approach for prediction of aerothermal loads - Progress in inviscid flow computations
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3. A finite element approach for solution of the 3D Euler equations
4. Flow-thermal-structural study of aerodynamically heated leading edges
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1. Error estimates and adaptive finite element methods;Engineering Computations;2001-08-01
2. Separation length in high-enthalpy shock/boundary-layer interaction;Physics of Fluids;2000
3. The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects;Journal of Fluid Mechanics;1997-07-10
4. Structured and unstructured grid adaptation schemes for numerical modeling of field problems;Applied Numerical Mathematics;1994-04
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