Damping of Axial Instabilities by Small-Scale Nozzles Under Cold-Flow Conditions
- 1 December 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 11 (12) , 812-820
- https://doi.org/10.2514/3.62182
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Experimental determination of three-dimensional liquid rocket nozzleadmittances.AIAA Journal, 1973
- Longitudinal mode acoustic losses in short nozzlesJournal of Sound and Vibration, 1972
- Application of Combustion Instability Technology to Solid-Propellant Rocket Motor ProblemsJournal of Spacecraft and Rockets, 1972
- Analysis of acoustic waves in a cold-flow rocket.Journal of Spacecraft and Rockets, 1969
- Design considerations for combustion stability.Journal of Spacecraft and Rockets, 1969
- Acoustic attenuation experiments on subscale, cold-flow rocket motors.AIAA Journal, 1967
- Effect of the transverse velocity component on the nonlinear behavior of short nozzles.AIAA Journal, 1966
- Experimental solid rocket combustion instabilitySymposium (International) on Combustion, 1965
- Interaction between Sound and Flow in Acoustic Cavities: Mass, Momentum, and Energy ConsiderationsThe Journal of the Acoustical Society of America, 1964
- Verification of Nozzle Admittance Theory by Direct Measurement of the Admittance ParameterARS Journal, 1961