Evaluation of absorption liners for suppression of combustion instability in rocket engines.
Author:
Affiliation:
1. United Aircraft Corporation Research Laboratories, East Hartford, Conn.
2. Pratt & Whitney Aircraft Division, West Palm Beach, Fla.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28594
Reference17 articles.
1. Studies of screeching combustion and pressure-wave, flamefront interaction
2. Effect of Nonlinear Losses on the Design of Absorbers for Combustion Instabilities
3. Acoustic Impedance of Small Orifices
4. The Acoustic Reactance of Small Circular Orifices
5. Acoustic Circulation Effects and the Nonlinear Impedance of Orifices
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