Numerical Simulation of Continuous Morphing Wing with Leading Edge and Trailing Edge Parabolic Flaps

Author:

Wang Ruochen1,Ma Xiaoping2,Zhang Guoxin3,Ying Pei4,Wang Xiangyu5

Affiliation:

1. Ph.D. Candidate, Institute of Engineering Thermophysics, Chinese Academy of Sciences, 11 Beisihuanxi Rd., Beijing 100190, China; Ph.D Candidate, Univ. of Chinese Academy of Sciences, 80 Zhongguancun East Rd., Beijing 100049, China.

2. Research Fellow, Institute of Engineering Thermophysics, Chinese Academy of Sciences, 11 Beisihuanxi Rd., Beijing 100190, China; Professor, Univ. of Chinese Academy of Sciences, 80 Zhongguancun East Rd., Beijing 100049, China (corresponding author).

3. Senior Engineer, Institute of Engineering Thermophysics, Chinese Academy of Sciences, 11 Beisihuanxi Rd., Beijing 100190, China.

4. Assistant Research Fellow, Institute of Engineering Thermophysics, Chinese Academy of Sciences, 11 Beisihuanxi Rd., Beijing 100190, China.

5. Engineer, Institute of Engineering Thermophysics, Chinese Academy of Sciences, 11 Beisihuanxi Rd., Beijing 100190, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference38 articles.

1. Effects of an Unsteady Morphing Wing with Seamless Side-Edge Transition on Aerodynamic Performance

2. Near Stall Unsteady Flow Responses to Morphing Flap Deflections

3. Allmaras S. R. and F. T. Johnson. 2012. “Modifications and clarifications for the implementation of the Spalart-Allmaras turbulence model.” In Proc. 7th Int. Conf. on Computational Fluid Dynamics (ICCFD7). Edwards AFB CA: Air Force Research Laboratory.

4. Morphing wings review: Aims, challenges, and current open issues of a technology;Ameduri S.;Proc. Inst. Mech. Eng. Part C J. Mech. Eng. Sci.,2020

5. A Review of Morphing Aircraft

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