Mean Flowfields in Axisymmetric Geometries with Swirl Combustor
Author:
Affiliation:
1. Oklahoma State University, Stillwater, Oklahoma
2. Dynamics Technology, Inc., Torrance, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.60127
Reference31 articles.
1. Prediction of swirling reacting flow in ramjet combustors
2. 4Rhode, D.L., Predictions and Measurements of Isothermal Flowfields in Axisymmetric Combustor Geometries, Ph.D. Thesis,Oklahoma State Univ., Stillwater, Okla. Dec.1981.
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