Porosity effect on supercritical airfoil drag reduction by shock wave/boundary layer control
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, NY
2. USAF, Eglin AFB, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1682
Reference8 articles.
1. Design of transonic airfoil sections using a similarity theory
2. Bahi, L., ROSS, J.M., and Nagamatsu, H.T. "Passive Shock WavdBoundsry Layer Control for Transonic Airfoil Drag Reduction,'' AIAA Paper No. 83-0137, Jan. 1983.
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