T-burner method of determining the acoustic admittance of burning propellants
Author:
Affiliation:
1. Lockheed Propulsion Company, Redlands, Calif
2. U S Naval Ordnance Testing Station, China Lake, Calif
3. University of Utah, Salt Lake City, Utah
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2477
Reference8 articles.
1. DYNAMIC CHARACTERISTICS OF SOLID PROPELLANT COMBUSTION
2. VIRTUAL SPECIFIC ACOUSTIC ADMITTANCE MEASUREMENTS OF BURNING SOLID PROPELLANT SURFACES BY A RESONANT TUBE TECHNIQUE
3. Interaction Between Sound and Flow: Stability of T-Burners
4. PARTICULATE DAMPING OF OSCILLATORY COMBUSTION
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