Internal Flow Temperature and Vorticity Dynamics Due to Transient Mass Addition
Author:
Affiliation:
1. Menoufia University, Shebin El-Kom, Egypt
2. University of Colorado, Boulder, Colorado 80309-0427
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12470
Reference45 articles.
1. 1Zhao, Q. "Nonlinear Acoustic Processes in Solid Rocket Engines," Ph.D. Dissertation, Mechanical Engineering Dept.Univ. of Colorado, Boulder, CO,Aug. 1994.
2. Acoustically generated vorticity in an internal flow
3. Unsteady vorticity generation and evolution in a model of a solid rocket motor
4. Three-dimensional, unsteady, acoustic-shear flow dynamics in a cylinder with sidewall mass addition
5. Coexisting acoustic-rotational flow in a cylinder with axisymmetric sidewall mass addition
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