Convergence of Two Internal Mean Flow Solutions for Spinning Rocket Motors
Author:
Affiliation:
1. Auburn University, Auburn, Alabama 36849
Funder
Division of Civil, Mechanical and Manufacturing Innovation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J058620
Reference33 articles.
1. Fluid flow in regions bounded by porous surfaces
2. Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.
3. On steady rotational high speed flows: the compressible Taylor–Culick profile
4. The Taylor-Culick profile with arbitrary headwall injection
5. Compressible integral representation of rotational and axisymmetric rocket flow
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