Computational analysis of buffet alleviation over a porous airfoil at high angle-of-attack-Reference-Cited by-同舟云学术

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Computational analysis of buffet alleviation over a porous airfoil at high angle-of-attack

Published:1994-06-20 Issue: Volume: Page:
ISSN:
Container-title:12th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Gillan Mark¹,Cooper Richard¹

Affiliation:

1. Belfast, Queen's Univ., United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1818

Reference34 articles.

1. 'Bahi, L."PassiveShockWaveIBoundaryLayer Controlfor Transonic Supercritical Drag Reduction", Ph.D. Thesis,RensselearPolytechnicInstitute, 1982.

2. 2Chen,C.L."Computation of TransonicFlow over Porous Airfoils", Ph.D. Thesis,University of Colorado,Boulder,CO,1986.

3. 5Gillan,M.A. "A ComputationalAnalysis of ViscousFlow Over Porous Aerofoils", Ph.D. Thesis, Aeronautical EngineeringDept.Queen's University of Belfast, 1993.

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