Code-to-Code Comparison of CFD/CSD Simulation for a Helicopter Rotor in Forward Flight
Author:
Affiliation:
1. NASA Ames Research Center
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3819
Reference21 articles.
1. Chimera simulations of multibladed rotors in high-speed forward flight with weak fluid-structure-coupling
2. 3Lim, J. W. and Strawn, R. C. “Prediction of HART II Rotor BVI Loading and Wake System Using CFD/CSD Loose Coupling,” AIAA Paper 2007-1281,Jan.2007.
3. 4Sankaran, V., Sitaraman, J., Wissink, A., Datta, A., Jayaraman, B., Potsdam, M., Mavriplis, D., Yang, Z., O’Brien, D., Saberi, H., Cheng, R., Hariharan,N.,andStrawn,R.“ApplicationoftheHeliosComputationalPlatformtoRotorcraftFlowfields,”AIAAPaper2010-1230,Jan.2010.
4. 5Nichols,R.,Trammel,R.,andBuning,P.“SolverandTurbulenceModelUpgradestoOVERFLOW2forUnsteadyandHigh-SpeedApplications,” AIAAPaper2006-2824,June2006.
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