Development of a Modeling and Simulation Tool for Rotorcraft/Ship Dynamic Interface Testing
VFS-F58-00052
6/11/2002
- Content
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This paper describes an ongoing effort to develop a high fidelity modeling and simulation tool to support rotorcraft/ship dynamic interface testing. The work include (1) enhancement of advanced finite state dynamic wake, free vortex wake, and panel modules for rotor wake/ship deck aerodynamic interaction; (2) integration of unsteady CFD and measured ship airwake data to couple with FLIGHTLAB, a comprehensive rotorcraft simulation program to provide a high fidelity rotorcraft/ship dynamic interface testing solution; (3) development of a rotorcraft shipboard operational limit prediction tool with coupled rotorcraft/ship aerodynamic interaction and integrated flight envelope analysis utilities.
- Citation
- He, C., Kang, H., Carico, D., and Long, K., "Development of a Modeling and Simulation Tool for Rotorcraft/Ship Dynamic Interface Testing," Forum 58 - Montreal, Canada 2002, Montreal, Canada, June 11, 2002, https://doi.org/10.4050/VFS-F58-00052.