Quantitative predictions of dump combustor flowfields
Author:
Affiliation:
1. Wright State University, Dayton, Ohio
2. Air Force Aero Propulsion Laboratory, Wright-Patterson AFB, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7857
Reference14 articles.
1. Fluid Dynamic Characterization of Sudden-Expansion Ramjet Combustor Flowfields x
2. Experimental Investigation of Subsonic Turbulent Flow Over Single and Double Backward Facing Steps
3. Kinetic Energy Methods
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1. Flow dynamics in low aspect ratio dump combustor;Propulsion and Power Research;2014-12
2. Identification of the Cold Flow Perturbation Sources in a Dump Combustor With a Tapered Exit;Journal of Fluids Engineering;2013-01-01
3. Predictions of swirling flow in sudden‐expansion dump combustor with flameholder side‐inlet using two‐step combustion model;International Journal of Numerical Methods for Heat & Fluid Flow;1999-11-01
4. Numerical simulations of acoustic-vortex interactions in a central-dump ramjet combustor;Journal of Propulsion and Power;1987-11
5. Numerical study of a ramjet dump combustor flowfield;AIAA Journal;1985-04
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