A parametric study of staged fuel injector configurations for scramjet applications
- 27 July 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Analytic and approximate boundary-fitted coordinate systems for fluid flow simulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical investigation of the perpendicular injector flow field in a hydrogen fueled scramjetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Initial wind tunnel tests at Mach 4 and 7 of a hydrogen-burning, airframe-integrated scramjetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- 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