Viscous-Inviscid Interaction for Transonic Wing-Body Configurations Including Wake Effects
- 1 July 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (7) , 915-923
- https://doi.org/10.2514/3.51149
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Computational transonic analysis for a supercritical transport wing-body configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- The Calculation of Three-Dimensional Turbulent Boundary Layers: Part II: Attachment-Line Flow on an Infinite Swept WingAeronautical Quarterly, 1967