Unsteady Numerical Simulation of the Mutual Disturbance between Propeller and Wing

Author:

QIAO Yuhang1,MA Dongli1,LI Zhi1

Affiliation:

1. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference22 articles.

1. 1) Lei, Z. and Kawamura, H.: Development of a Solar-Powered Unmanned Aerial Vehicle, AIAA 2014-0539, 52nd Aerospace Sciences Meeting, National Harbor, Maryland, 2014.

2. 2) Nickol, C. L., Guynn, M. D., Kohout, L. L., and Ozoroski, T. A.: High Altitude Long Endurance UAV Analysis of Alternatives and Technology Requirements Development, NASA, USA, Tech. Rep. Report No. NASA/TP-2007-214861, 2007.

3. 3) Romeo, G., Frulla, G., Cestino, E., and Corsino, G.: HELIPLAT: Design, Aerodynamic, Structural Analysis of Long-endurance Solar-powered Stratospheric Platform, J. Aircraft, 41 (2004), pp. 1505–1520.

4. 4) Li, B., Liang, D., and Huang, G.: Propeller Slipstream Effects on Aerodynamic Performance of Turbo-prop Airplane Based on Equivalent Actuator Disk Model, Acta Aeronautica Astronautica Sinica, 29 (2008), pp. 845–852.

5. 5) E, Q., Yang, G., Li, F., and He, Z. D.: Numerical Calculation of Interaction of Propeller Slipstream on Flowfield over a Complete Aircraft, Acta Aeronautica Astronautica Sinica, 17 (1996), pp. 439–442.

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