High aspect ratiowing design: Optimal aerostructural tradeoffs for the next generation of materials

52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014

Volumn , Issue , 2014, Pages

  Kennedy, Graeme J ^a   Kenway, Gaetan W ^a   Martins, Joaquim R R A ^b  

^a Georgia Institute of Technology   (United States)

^b UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; CARBON NANOTUBES; FLEXIBLE WINGS; OPTIMIZATION; TRANSPORT AIRCRAFT;

AERO-STRUCTURAL OPTIMIZATION; BUCKLING CONSTRAINTS; CARBON FIBER REINFORCED COMPOSITE; CARBON-NANOTUBE COMPOSITES; COMPUTATIONAL MODEL; LARGE TRANSPORT AIRCRAFT; MATERIAL TECHNOLOGIES; MINIMUM FUEL BURNS;

DESIGN;

EID: 84902782060     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (35)

1. S. Balay, W. D. Gropp, L. C. McInnes, and B. F. Smith. Efficient management of parallelism in object oriented numerical software libraries. In E. Arge, A. M. Bruaset, and H. P. Langtangen, editors, Modern Software Tools in Scientific Computing, pages 163-202. Birkhäuser Press, 1997.
2. S. Brown. Displacement extrapolation for CFD+CSM aeroelastic analysis. In 38th Structures, Structural Dynamics, and Materials Conference, April 1997. doi:10.2514/6.1997-1090. AIAA97-1090.
3. I. R. Chittick and J. R. R. A. Martins. An asymmetric suboptimization approach to aerostructural optimization. Optimization and Engineering, 10(1):133-152, Mar. 2009. doi:10.1007/s11081-008-9046-2.
4. P. E. Gill, W. Murray, and M. A. Saunders. SNOPT: An SQP algorithm for large-scale constrained optimization. SIAM Review, 47(1):99-131, 2005. doi:10.1137/S0036144504446096.
5. B. Grossman, R. T. Haftka, P.-J. Kao, D. M. Polen, and M. Rais-Rohani. Integrated aerodynamic-structural design of a transport wing. Journal of Aircraft, 27(12):1050-1056, 1990. doi:10.2514/3.45980.
6. E. J. Hopkins. Charts for predicting turbulent skin friction from the van Driest method (II). Technical Report TN D-6945, NASA, October 1972.
7. A. Jameson. Computational aerodynamics for aircraft design. Science, 245:361-371, 1989.
8. R. M. Jones. Mechanics of Composite Materials. Technomic Publishing Co., 1996.
9. C. V. Jutte, B. K. Stanford, C. D. Wieseman, and J. B. Moore. Aeroelastic tailoring of the NASA common research model via novel material and structural configurations. In Proceedings of the SciTech Conference, National Harbor, MD, January 2014.
10. J. Katz and A. Plotkin. Low-Speed Aerodynamics. McGraw-Hill Inc., 1991.
11. G. J. Kennedy and J. R. R. A. Martins. Parallel solution methods for aerostructural analysis and design optimization. In Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, Fort Worth, TX, September 2010. AIAA 2010-9308.
12. G. J. Kennedy and J. R. R. A. Martins. A comparison of metallic and composite aircraft wings using aerostructural design optimization. In 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Indianapolis, IN, Sep. 2012. AIAA-2012-5475.
13. G. J. Kennedy and J. R. R. A. Martins. A laminate parametrization technique for discrete ply angle problems with manufacturing constraints. Structural and Multidisciplinary Optimization, 48(2):379-393, August 2013. doi:10.1007/s00158-013-0906-9.
14. G. K. W. Kenway and J. R. R. A. Martins. Multi-point high-fidelity aerostructural optimization of a transport aircraft configuration. Journal of Aircraft, 2013. doi:10.2514/1.C032150. (In press).
15. G. K.W. Kenway, G. J. Kennedy, and J. R. R. A. Martins. A scalable parallel approach for high-fidelity steady-state aeroelastic analysis and adjoint derivative computations. AIAA Journal, 2012. (In press).
16. I. Kroo. Aircraft design: Synthesis and analysis, November 2013. URL http://adg.stanford.edu/aa241/AircraftDesign.html.
17. I. M. Kroo. Drag due to lift: Concepts for prediction and reduction. Annual Review of Fluid Mechanics, 33:587-617, Nov. 2000.
18. Z. Lyu and J. R. R. A. Martins. Aerodynamic design optimization studies of a blended-wing-body aircraft. Journal of Aircraft, 2014. (In press).
19. Z. Lyu, G. K. Kenway, C. Paige, and J. R. R. A. Martins. Automatic differentiation adjoint of the Reynolds-averaged Navier-Stokes equations with a turbulence model. In 21st AIAA Computational Fluid Dynamics Conference, San Diego, CA, Jul 2013. doi:10.2514/6.2013-2581.
20. C. A. Mader and J. R. R. A. Martins. Stability-constrained aerodynamic shape optimization of flying wings. Journal of Aircraft, 50(5):1431-1449, September 2013. doi:10.2514/1.C031956.
21. C. A. Mader, J. R. R. A. Martins, J. J. Alonso, and E. van der Weide. ADjoint: An approach for the rapid development of discrete adjoint solvers. AIAA Journal, 46(4):863-873, Apr. 2008. doi:10.2514/1.29123.
22. B. Malone and W. Mason. Multidisciplinary optimization in aircraft design using analytic technology models. Journal of Aircraft, 32(2):431-438, mar-apr 1995. doi:10.2514/3.46734.
23. J. R. R. A. Martins and J. T. Hwang. Review and unification of methods for computing derivatives of multidisciplinary computational models. AIAA Journal, 51(11):2582-2599, 2013. doi:10.2514/1.J052184.
24. J. R. R. A. Martins and A. B. Lambe. Multidisciplinary design optimization: A survey of architectures. AIAA Journal, 51(9): 2049-2075, Sep 2013. doi:10.2514/1.J051895.
25. J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther. High-fidelity aerostructural design optimization of a supersonic business jet. Journal of Aircraft, 41(3):523-530, 2004. doi:10.2514/1.11478.
26. J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther. A coupled-adjoint sensitivity analysis method for high-fidelity aerostructural design. Optimization and Engineering, 6(1):33-62, Mar. 2005. doi:10.1023/B:OPTE.0000048536.47956.62.
27. R. E. Perez, P.W. Jansen, and J. R. R. A. Martins. pyOpt: a Python-based object-oriented framework for nonlinear constrained optimization. Structural and Multidisciplinary Optimization, 45(1):101-118, January 2012. doi:10.1007/s00158-011-0666-3.
28. N. M. K. Poon and J. R. R. A. Martins. An adaptive approach to constraint aggregation using adjoint sensitivity analysis. Structural and Multidisciplinary Optimization, 34(1):61-73, 2007. doi:10.1007/s00158-006-0061-7.
29. Y. Saad and M. H. Schultz. GMRES: A generalized minimal residual algorithm for solving nonsymmetric linear systems. SIAM Journal on Scientific and Statistical Computing, 7(3):856-869, 1986. doi:10.1137/0907058.
30. W. J. Stroud and N. Agranoff. Minimum mass design of filamentary composite panels under combined loads: Design procedure based on simplified buckling equations. Technical report, NASA Langley Research Center, Hampton, VA 23665, October 1976.
31. E. van der Weide, G. Kalitzin, J. Schluter, and J. J. Alonso. Unsteady turbomachinery computations using massively parallel platforms. In Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 2006. AIAA 2006-0421.
32. J. C. Vassberg. A unified baseline grid about the common research model wing-body for the fifth aiaa cfd drag prediction workshop. In 29th Applied Aerodynamics Conference, Honolulu, Hawaii, June 2011. doi:10.2514/6.2011-3508. AIAA 2011-3508.
33. S. Venkatamaran and R. T. Haftka. Structural optimization complexity: what has Moore's law done for us? Structural and Multidisciplinary Optimization, 28:375-387, 2004.
34. V. B. Venkayya. Structural optimization: A review and some recommendations. International Journal for Numerical Methods in Engineering, 13(2):203-228, 1978. doi:10.1002/nme.1620130202.
35. S. Wakayama and I. Kroo. Subsonic wing planform design using multidisciplinary optimization. Journal of Aircraft, 32(4): 746-753, 1995. doi:10.2514/3.46786.