A new finite element approach for prediction of aerothermal loads - Progress in inviscid flow computations
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Old Dominion University, Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1533
Reference23 articles.
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. STABILIZED FLUX-BASED FLOW / THERMAL FINITE ELEMENT REPRESENTATIONS WITH APPLICATIONS TO CONVECTIVELY COOLED STRUCTURES;Journal of Thermal Stresses;2002-03
2. Adaptive finite element analysis of hypersonic laminar flows for aerothermal load predictions;Journal of Thermophysics and Heat Transfer;1991-07
3. Adaptive quadrilateral and triangular finite-element scheme for compressible flows;AIAA Journal;1990-01
4. Flow-thermal-structural study of aerodynamically heated leading edges;Journal of Spacecraft and Rockets;1989-07
5. Explicit Lax-Wendroff/Taylor-Galerkin second-order accurate formulations involving flux representations for effective finite element thermal modeling/analysis;27th Aerospace Sciences Meeting;1989-01-09
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