Wing's optimization design using serial and parallel computations based on N-S equations

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 34, Issue 2, 2008, Pages 127-130

  Wen, Jianhua ^a   Zhu, Ziqiang ^a   Wu, Zongcheng ^a   Chen, Zemin ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Navier stokes equations; Optimization design; Parallel computation; Wing design

Indexed keywords

AEROSPACE ENGINEERING; AIRCRAFT PARTS AND EQUIPMENT; ASPECT RATIO; FLOW FIELDS; MACH NUMBER; NAVIER STOKES EQUATIONS; OPTIMIZATION;

LIFT DRAG RATIO; NONLINEAR DISTRIBUTION; OPTIMIZATION DESIGN; PARALLEL COMPUTATION; POWELL METHOD; SERIAL COMPUTATION; WING DESIGN;

WINGS;

EID: 40949144461     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (9)

1. Van der Velden A, Forbrich D. Use of aerodynamic shape optimization for a large transonic aircraft[R]. AIAA 97-2274, 1997.
2. Van der Velden A, Von Reith D. Multi-disciplinary SCT design al deutsche aerospace airbus[C]//Proceedings of the 7th European Aerospace conference. Toulouse: [s. n.], 1994.
3. Takahashi T T, Coopersmith R M. Wing section design for a long-range hydrofoil transport[R]. AIAA 2002-0832, 2002.
4. Sobieczky H. New design concept for high speed air transports[C]//Sobieczky H. CISM Cours and Lectures No.366. New York: Springer Wien, 1997.
5. Zhu Ziqiang, Wu Zongcheng. Aerodynamics for modern aircraft design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2005 (in Chinese).
6. +[R], AIAA, 95-1701, 1995.
7. Li Yan, Zhu Ziqiang, Wang Xiaolu, el al. Optimization design of wing's thickness and twist angle using Euler equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(3): 269-272(in Chinese).
8. Burdges K P, Hinson B L. Transport wing and far field lest data on a high aspect ratio wing for three dimensional computational method evaluation[R]. AGARD-AR-138, 1979.
9. Burdges K P, Hinson B L. Transport wing and far field test data on a moderate aspect ratio wing for three dimensional computational method evaluation[R]. AGARD-AR-138, 1979.