Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets
Author:
Affiliation:
1. University of Naples Federico II, 80125 Naples, Italy
2. Polytechnic University of Turin, 10129 Turin, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference22 articles.
1. Nonlinear rocket motor stability prediction: Limit amplitude, triggering, and mean pressure shift
2. Modeling of Hybrid Rocket Low Frequency Instabilities
3. Acoustics, Vortex Shedding, and Low-Frequency Dynamics Interaction in an Unstable Hybrid Rocket
4. Dynamic Modeling of Hybrid Rocket Combustion
5. Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors
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