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- W4283738943 abstract "Abstract: Space vehicles are subjected to significant dynamic pressure loads when their rocket propulsion systems are in use during flying missions. During the aerodynamic and launch phases, launch vehicles, payloads, and their parts are subjected to extremely high random acoustic loads. The noise from the engine exhaust gas, aerodynamic boundary layer noise, transonic buffering, structure-borne vibration, engine thrust fluctuation, etc. is the source of these loads, which also result in a secondary acoustic load. When the vehicle is lifting off and traveling at a speed greater than Mach number, acoustic stresses to the spacecraft and payload are very harsh and significant. This loading causes the structure to vibrate randomly, which could be dangerous for some vehicle parts, avionics, propulsion systems, and payloads like satellites. This paper discusses the vibration of the structure subjected to acoustic excitation on a diffuse acoustic field and the software used for the analysis." @default.
- W4283738943 created "2022-07-02" @default.
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- W4283738943 date "2022-06-30" @default.
- W4283738943 modified "2023-10-18" @default.
- W4283738943 title "A Review on Vibro-Acoustic Analysis of a Launch Vehicle Structure" @default.
- W4283738943 doi "https://doi.org/10.22214/ijraset.2022.44873" @default.
- W4283738943 hasPublicationYear "2022" @default.
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