38th Aerospace Sciences Meeting and Exhibit: 10-13 January 2000, Reno, NV. |
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ablation acoustic oscillations aeroelastic Aeronautics and Astronautics Aerospace Sciences Meeting AIAA air preheat American Institute angle axial behavior boundary buck converter burner calculated canard chamber Combustion Institute combustor computational configuration constraints convective counterflow density design metric diffusion flame DRAMR effects energy equations equivalence ratio exit expansion experimental data extinction Figure fire flame speed flame structure flashover flow field fluid fluid solution frequency fuel function gradient heat flux heat release ignition incineration increase input instability Institute of Aeronautics interaction International Space Station investigated laminar burning velocities Leonid linear Mach number mass maximum measured mechanisms mesh meteor meteoroid method microgravity mixture NASA nonpremixed nozzle optimization parameters partially premixed flames pilot flame predicted preheat premixed flames present profiles pylon radiation reaction zone sensitivity shock tube simulation solution strain rate surface temperature thermal tube turbulent umbilical values vapor variables variation vortex
Bibliographic information
| Title | 38th Aerospace Sciences Meeting and Exhibit: 10-13 January 2000, Reno, NV. Volume 11 of 38th Aerospace Sciences Meeting and Exhibit: 10-13 January 2000, Reno, NV, American Institute of Aeronautics and Astronautics |
| Contributor | American Institute of Aeronautics and Astronautics |
| Publisher | American Institute of Aeronautics and Astronautics, 2000 |
| Original from | Pennsylvania State University |
| Digitized | Jun 24, 2009 |
| Export Citation | BiBTeX EndNote RefMan |