Computation of the asymmetric vortex pattern for bodies of revolution
- 11 January 1982
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Numerical simulation of wing-fuselage interferencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Pressure measurements on an ogive-cylinder at high angles of attack with laminar, transitional, or turbulent separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Computation of supersonic viscous flows over ogive-cylinders at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- On implicit finite-difference simulations of three-dimensional flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Approximate Method for Estimating Wake Vortex StrengthAIAA Journal, 1974
- The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidenceJournal of Fluid Mechanics, 1971