Aeroelastic Analysis for the High Altitude Propeller by Using Fluid-Structure Interaction Method
Author:
Affiliation:
1. Academy of Opto-Electronics, Chinese Academy of Science
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/16/3/16_236/_pdf
Reference10 articles.
1. 1) Westmoreland, W.S., Tramel, R.W., and Barber, J.: Modeling Propeller Flow-fields Using CFD, 46th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2008-402, 2008.
2. 2) Sodja, J., Stadler, D., and Kosel T.: Computational Fluid Dynamics Analysis of an Optimized Load-Distribution Propeller, J. Aircraft, 49 (2012), pp. 955–961.
3. 3) Goble, B. D. and Hooker, J. R.: Validation of an Unstructured Grid Euler / Navier-Stokes Code on a Full Aircraft with Propellers, 39th AIAA Aerospace Sciences Meeting & Exhibit, AIAA Paper 2001-1003, 2001.
4. 4) Xu, H., Ye, Z., and Shi, A.: Numerical Study of Propeller Slipstream Based on Unstructured Overset Grids, J. Aircraft, 49 (2012), pp. 384–389.
5. 5) Sudhir, S. Y. B., Bhargavi, R. I., and Durga, R. K.: Stress Analysis of Helicopter Composite Blade Using Finite Element Analysis, International Journal of Engineering Research & Technology, 2 (2013), pp. 1291–1299.
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