Multi-disciplinary optimization and numerical simulation in civil aircraft design

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 28, Issue 1, 2007, Pages 1-13

  Zhu, Zi Qiang ^a   Wang, Xiao Lu ^a   Wu, Zong Cheng ^a   Chen, Ze Min ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Civil transport design; Multi disciplinary design optimization; Numerical simulation

Indexed keywords

AIRPORT PASSENGER TRANSPORTATION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; OPTIMIZATION; PRESSURE DISTRIBUTION;

CIVIL TRANSPORT DESIGN; MULTI-DISCIPLINARY DESIGN OPTIMIZATION;

AIRCRAFT;

EID: 34249851459     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Review

References (35)

1. Zhu Z Q, Wu Z C. Aerodynamics for modern aircraft design[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2005. (in Chinese)
2. Szodruch J, Hilbig R. Building the future aircraft design for the next century[R]. AIAA 98-0135, 1998.
3. Raj P. Aircraft design in 21st century: implications for design methods[R]. AIAA 98-2895, 1998.
4. Vos J B, Rizzi A, Darracq D, et al. Navier-Stokes solves in European aircraft design[J]. Progress in Aerospace Sciences, 2002, 8, 601-697.
5. Hajela P. Soft computing in multi-disciplinary aerospace design-new directions for research[J]. Progress in Aerospace Sciences, 2002, 38: 1-21.
6. Zang T A, Green L L. Framework requirements for MDO application development[R]. AIAA 98-4740, 1998.
7. Giesing J P, Barthelemy J F M. A summary of industry MDO applications and needs[R]. AIAA 98-4737, 1998.
8. Sobieszczanki-Sobieski J. Multi-disciplinary design optimization: an emerging new engineering discipline in advances in structural mechanics[M]. Herkovitch J edited. Kluwer Academic Publishers, Doordrecht, 1995, 488-496.
9. Le Doux S T, Herling W W, Fatta G J. MDOPT-a multi-disciplinary design optimization system using higher order analysis codes[R]. AIAA 2004-4567, 2004.
10. Morris A J. MOB: a European distributed multi-disciplinary design and optimization project[R]. AIAA 2002-5444, 2002.
11. van der Velden A, Kelm R, Kokan D, et al. Application of MDO to large subsonic transport aircraft[R]. AIAA 2000-0844, 2000.
12. Zhang K S. A new method for optimum allocation of design requirements in aircraft conceptual design[J]. Chinese Journal of Aeronautics, 2006, 19(3): 203-211.
13. Wang G L, Wu Z. System frame research on aircraft conceptual design platform based on virtual prototyping[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(2): 162-167. (in Chinese)
14. Liu G, Wang X R, Jia R Z. Technique for dynamic virtual prototype of aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(5): 550-555. (in Chinese)
15. He L S, Wang S H, Zhang Y Z. The new algorithm for aircraft Multi-disciplinary integrated design[J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(5): 465-469. (in Chinese)
16. Chen Q F, Dai J H, Li X B. Multi-disciplinary design optimization based on distributed coevolution-algorithm and application in missile design[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(3): 245-248.
17. Wang G L, Sun Y D, Wu Z. Rapid uniform aliform component modeling based on parameter in conceptual aircraft design[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(6): 575-578. (in Chinese)
18. Huang J, Wu Z, Sun H Z, et al. Recent development in conceptual/preliminary design optimization of aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(6): 481-487.
19. Yu X Q, Ding Y L. Multi-disciplinary design optimization a survey of its algorithms and applications to aircraft design[J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(1): 1-6.
20. Johnson F T, Tinoco E N, Yu N J. Thirty years of development and application of CFD at Boeing commercial airplanes[R]. AIAA 2003-3439, 2003.
21. Nield B N. An overview of the Boeing 777 high lift aerodynamic design[J]. Aero J, 1995, 11: 361-371.
22. Zhu Z Q, Chen Y C, Wu Z C, et al. Numerical simulation of high lift system configuration[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(3): 257-262. (in Chinese)
23. Rogers S E, Roth K, Cao H V, et al. Computation of viscous flow for a Boeing 777 aircraft in landing configuration[J]. Journal of Aircraft, 2001, 38(6): 1060-1068.
24. Quest J, Wright M C, Hansen H, et al. First measurement on an airbus high lift configuration at ETW up to flight Reynolds number[R]. AIAA 2002-0423, 2002.
25. Hansen H, Thiede P, Moens F, et al. Overview about the European high lift research programme EUROLIFT[J]. AIAA 2004-767, 2004.
26. Fang B R, et al. Airpline aerodynamic design[M]. Beijing: Aviation Industry Press, 1997. (in Chinese)
27. Ytterstrom A, Axelsson E. Hammershock calculations in the air intake of JAS 39 Gripen using dual timestepping[R]. AIAA 99-3113, 1999.
28. Jou W H, Huffman W P, Young D P, et al. Practical considerations in aerodynamic design optimization[R]. AIAA 95-1730, 1995.
29. Li P, Om D. Design application in the industry[C]//IUTAM symposium transsonicum IV. Kluwer Academic Publishers, 2003: 231-238.
30. Jou W H. Towards industrial strength Navier-Stokes codesa revisit in frontiers of computational fluid dynamics[M]. Singapore: World Scientific, 1998: 383-394.
31. Jameson A. A perspective on computational algorithms for aerodynamic analysis and design[J]. Progress in Aerospace Sciences, 37, 197-243, 2001.
32. Wang X L, Zhu Z Q, Liu Z, et al. Bi-point (BP)/bi-objective (BO) optimization design of airfoil using N-S equations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(5): 503-507. (in Chinese)
33. Wang X L, Zhu Z Q. Hybrid optimization design of high performance unmanned aerial vehicle airfoil[J]. Acta Aeronautica et Astronautica Sinica (under reviewing, in Chinese)
34. Li Y, Zhu Z Q, Wang X L, et al. Optimization design of wing's thickness and twist angle using Euler equations[J]. Journal of Beijing University of Aeronautics and Astronautics (accepted, in Chinese)
35. Wen J H, Zhu Z Q, Wang X L, et al. Optimization design of wing's thickness and twist angle using serial and parallel computations based on N-S equations[J]. Journal of Beijing University of Aeronautics and Astronautics (under reviewing, in Chinese)