Investigation of scramjet injection strategies for high Mach number flows
| Autor: | David W. Riggins, Charles R. McClinton, Robert D. Bittner, R. C. Rogers |
|---|---|
| Rok vydání: | 1995 |
| Předmět: |
Physics
Jet (fluid) Mechanical Engineering Aerospace Engineering Thrust Injector Inflow Mechanics law.invention Vortex symbols.namesake Fuel Technology Mach number Space and Planetary Science law Physics::Space Physics symbols Mass flow rate High Energy Physics::Experiment Scramjet Astrophysics::Galaxy Astrophysics |
| Zdroj: | Journal of Propulsion and Power. 11:409-418 |
| ISSN: | 1533-3876 0748-4658 |
| DOI: | 10.2514/3.23859 |
| Popis: | A method for estimating the axial distribution of thrust performance potential in a supersonic combustor is described. A complementary technique for illustrating the spatial evolution and distribution of thrust potential and loss mechanisms in reacting flows is developed. A wall jet case and swept ramp injector case for Mach 17 and Mach 13.5 flight enthalpy inflow conditions, respectively, are numerically modeled and analyzed using these techniques. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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