Experimental Study of Acoustic Velocity Effects on Simulated Solid Fuel Pyrolysis
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.273
Reference18 articles.
1. Exploiting hydrodynamic instabilities. Resonant heat transfer enhancement
2. Numerical investigation of incompressible flow in grooved channels. Part 2. Resonance and oscillatory heat-transfer enhancement
3. Heat transfer enhancement in the oscillating turbulent flow of a pulse combustor tail pipe
4. Heat/Mass Transfer from a Cylinder in the Strongly Oscillating Flow of a Pulse Combustor Tailpipe
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