Dynamic loads on twin jet exhaust nozzles due to shock noise
- 1 September 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (9) , 728-729
- https://doi.org/10.2514/3.45370
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Dynamic stability of flexible forward swept wing aircraftJournal of Aircraft, 1983
- Screech suppression in supersonic jetsAIAA Journal, 1983
- Aeroelastic divergence of unrestrained vehiclesJournal of Aircraft, 1981
- The noise from unheated supersonic jets in simulated flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Recent observations including temperature dependence of axisymmetricjet screechAIAA Journal, 1975
- In-flight shock cell noiseJournal of Sound and Vibration, 1970
- The Static Aeroelastic Deformation of Slender ConfigurationsAeronautical Quarterly, 1961
- On the Mechanism of Choked Jet NoiseProceedings of the Physical Society. Section B, 1953