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Design of a wing shape for study of hypersonic crossflow transition in flight

  • Published:1992-01 Issue:1-4 Volume:3 Page:115-130
  • ISSN:0956-0521
  • Container-title:Computing Systems in Engineering
  • language:en
  • Short-container-title:Computing Systems in Engineering

Author:

Godil A.,Bertelrud A.

Publisher

Elsevier BV

Subject

General Engineering

Reference13 articles.

1. COSAL—a black-box compressible stability analysis code for transition prediction in three-dimensional boundary layers;Malik,1982

2. The linear stability of three-dimensional boundary layers over axisymmetric bodies at incidence;Spall;AIAA Paper No. 91-1640,1991

3. Application of linear stability theory in laminar flow design;Iyer,1991

4. Aerodynamic design of Pegasus®;Mendenhall;AIAA Paper No. 91-0190,1991

5. Pegasus® flight results;Mossier,1990

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. Thermal Heating and Design;Design Methodologies for Space Transportation Systems;2001-01-01

2. Pegasus wing-glove experiment to document hypersonic crossflow transition - Measurement system and selected flight results;38th Aerospace Sciences Meeting and Exhibit;2000-01-10

3. A hypersonic flight test to document laminar/turbulent transition;9th International Space Planes and Hypersonic Systems and Technologies Conference;1999-08-22

4. Computational Aerothermodynamic Design Issues for Hypersonic Vehicles;Journal of Spacecraft and Rockets;1999-01

5. Computational aerothermodynamic design issues for hypersonic vehicles;32nd Thermophysics Conference;1997-06-23
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