Author:
Malo-Molina Faure,Gaitonde Datta,Ebrahimi Houshang,Ruffin Stephen
Publisher
American Institute of Aeronautics and Astronautics
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Three Dimensional Analysis of a Fully Coupled Hypersonic Air-breathing Inlet-Combustor Flowpath;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
2. Exploratory RANS and LES simulations of transient supersonic combustor flow;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. High Fidelity Flowpath Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05