Preferred frequency oscillatory combustion of solid propellants
Author:
Affiliation:
1. U. S. Naval Ordnance Test Station, China Lake, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2539
Reference12 articles.
1. The unsteady burning of cordite
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1. References;Theory of Solid‐Propellant Nonsteady Combustion;2020-08-28
2. Mean Burning Rate Variation in Composite Propellant Combustion Due to Longitudinal Acoustic Oscillations;Journal of Propulsion and Power;2020-07
3. Combustion of solid propellants at low pressure;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24
4. L* Instability;Nonsteady Burning and Combustion Stability of Solid Propellants;1992-01-01
5. Effects of a melt-layer on the L instability in solid-propellant rockets. I - Linear study;27th Aerospace Sciences Meeting;1989-01-09
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