Erratum on Higher Mean-Flow Approximation for a Solid Rocket Motor with Radially Regressing Walls
Author:
Affiliation:
1. University of Tennessee Space Institute, Tullahoma, Tennessee 37388
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40061
Reference5 articles.
1. Higher Mean-Flow Approximation for Solid Rocket Motors with Radially Regressing Walls
2. On laminar flow through a uniformly porous pipe
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