Airfoil design method using the Navier-Stokes equations
- 1 March 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (3) , 216-224
- https://doi.org/10.2514/3.46015
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Inverse airfoil design using the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Two-dimensional transonic aerodynamic design methodAIAA Journal, 1987
- Analysis of viscous transonic flow over airfoil sectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Iterative three-dimensional transonic wing design using integral equationsJournal of Aircraft, 1985
- Numerical solution of unsteady viscous flow past rotor sectionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Design using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A combined direct/inverse three-dimensional transonic wing design method for vector computersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A Subsonic Panel Method for Iterative Design of Complex Aircraft ConfigurationsJournal of Aircraft, 1982
- Design of supercritical swept wingsAIAA Journal, 1982
- An Implicit Factored Scheme for the Compressible Navier-Stokes EquationsAIAA Journal, 1978