Drag prediction for military aircraft using CFD
Author:
Affiliation:
1. Northrop Grumman Corp., Pico Rivera, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-383
Reference11 articles.
1. Tysinger, T. L. and Caughey, D. A. "Implicit Multigrid Algorithm for the Navier Stokes Equations"AIAA Paper9l-0242, Jan1991. t ,
2. Tysinger, T. L. and Caughey,D. A. "Implicit Multigrid Algorithm for the Navier Stokes Equations"AIAA Paper9l-0242,Jan1991.
3. Menter, F. R. "Zonal Two-Equation k-o Turbulence Models for Aerodynamic Flows0022, AIAA Paper93-2906,July 1993.
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1. Comparison of predicting drag methods using computational fluid dynamics in 2d/3d viscous flow;Science in China Series E: Technological Sciences;2007-10
2. An assessment of CFD prediction for ONERA Model M5 configuration using CASPER;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14
3. Improvement of Drag Prediction for Transonic Transport Aircraft Configuration Using Hybrid Unstructured Navier-Stokes Solver.;JSME International Journal Series B;2002
4. An assessment of CFD prediction of drag and other longitudinal characteristics;39th Aerospace Sciences Meeting and Exhibit;2001-01-08
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