Scaling of Rocket Nozzle Admittances
- 1 July 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (7) , 918-923
- https://doi.org/10.2514/3.60470
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Damping of Axial Instabilities by Small-Scale Nozzles Under Cold-Flow ConditionsJournal of Spacecraft and Rockets, 1974
- Experimental and theoretical determination of the admittances of a family of nozzles subjected to axial instabilitiesJournal of Sound and Vibration, 1973
- Longitudinal mode acoustic losses in short nozzlesJournal of Sound and Vibration, 1972
- 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