Computation of steady and unsteady control surface loads in transonic flow
Author:
Affiliation:
1. Douglas Aircraft Co., Long Beach, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-935
Reference14 articles.
1. Further comparisons of interactive boundary-layer and thin-layer Navier-Stokes procedures
2. An Interactive Scheme for Three-Dimensional Transonic Flows
3. An interactive three-dimensional boundary-layer method for transonicflow over swept wings
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4. Control surface effectiveness in the transonic regime;7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;1998-08-22
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