Transonic airfoil design procedure utilizing a Navier-Stokes analysis code
- 1 March 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (3) , 353-359
- https://doi.org/10.2514/3.9629
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Iterative three-dimensional transonic wing design using integral equationsJournal of Aircraft, 1985
- Numerical optimization design of advanced transonic wing configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Inverse Transonic Wing Design MethodJournal of Aircraft, 1981
- Transonic Wing Design Using Potential-Flow Codes - Successes and FailuresSAE International Journal of Advances and Current Practices in Mobility, 1981
- Artificial viscosity method for the design of supercritical airfoils. [Analysis code H]Published by Office of Scientific and Technical Information (OSTI) ,1979
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- Transonic Airfoil Analysis and Design Using Cartesian CoordinatesJournal of Aircraft, 1976