Preliminary aerostructural optimization of a large business jet

Journal of Aircraft

Volumn 44, Issue 5, 2007, Pages 1422-1438

  Piperni, P ^a,c,d   Abdo, M ^a,d,e   Kafyeke, F ^a,d,f   Isikveren, Askin T ^b,g  

^a BOMBARDIER AEROSPACE   (Canada)

^b UNIVERSITY OF BRISTOL   (United Kingdom)

^c High Speed Aerodynamics   (Canada)

^d AIAA   (United States)

^e NCAP Technical and Aerodynamics

^f Advanced Aerodynamics and Strategic Technology

^g Research and Teaching Group   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DRAG; OPTIMIZATION; STRUCTURAL ANALYSIS; SYSTEMS ANALYSIS;

AEROSTRUCTURAL OPTIMIZATION; AIRCRAFT DESIGN; OPERATING ECONOMICS; REAR-MOUNTED ENGINES;

AERODYNAMICS;

EID: 36349013321     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.26989     Document Type: Article

References (43)

1. Ashely, H., "On Making Things the Best-Aeronautical Uses of Optimization," AIAA Aircraft Systems and Technology Conference, AIAA, New York, Aug. 1981, pp. 1-32; also AIAA Paper 81-1738.
2. Kafyeke, F., and Mavriplis, F., CFD for the Aerodynamic Design of Bombardier's Global Express, AIAA Paper 1997-2269, 1997.
3. Goritschnig, G., Isikveren, A., Lamothe, M., and Munger, E., "The Evolution of Civil Aircraft Design at Bombardier: A Historical Perspective," CASI Conference Proceedings, [CD-ROM], Canadian Aeronautics and Space Institute, Ottawa, Toronto, 2003, pp. 1-14.
4. Kroo, I., and Manning, V., "Collaborative Optimization: Status and Directions," AIAA Paper 2000-4721,2000, pp. 1-11.
5. Allwright, S., "Technical Data Management for Collaborative MultiDiscipline Optimization," AIAA Paper 96-4160, 1996.
6. Sobieski, J., and Haftka, R. T., "Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments," AIAA Paper 96-0711, 1996.
7. Balling, R. J., and Wilkinson, C. A., "Execution of Multidisciplinary Design Optimization Approaches on Common Test Problems," 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA, Reston, VA, 1996, pp. 421-437; also AIAA Paper 96-4033-CP.
8. Morris, A. J., and Gantois, K., "Combined MDO Optimization Including Drag, Mass and Manufacturing Information," 7th AIAA/ USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA, Reston, VA, Sept. 1998, pp. 1724-1732; also AIAA Paper 98-4777.
9. Van der Velden, A., KeIm, R., Kokan, D., and Mertens, J., "Application of MDO to Large Subsonic Transport Aircraft," AIAA Paper 2000-0844, 2000.
10. Prandtl, L., "Applications of Modern Hydrodynamics to Aeronautics," translated as NACA Rept. 116 (original sources dated 1918-1920).
11. Jones, R. T., "The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having Given Lift and Root Bending Moment," NASA TN-2249, 1950.
12. Jones, R. T., and Lasinski, T., "Effect of Winglets on the Induced Drag of Ideal Wing Shapes," NASA TM-81230, 1980.
13. McGeer, T., "Wing Design for Minimum Drag with Practical Constraints," Journal of Aircraft, Vol. 21, Nov. 1984, pp. 879-886.
14. Craig, A., and McLean, J., "Spanload Optimization for Strength Designed Lifting Surfaces," AIAA Paper 88-2512, 1988.
15. Wakayama, S., and Kroo, I., "Subsonic Wing Planform Design Using Multidisciplinary Optimization," Journal of Aircraft, Vol. 32, No. 4, July-Aug. 1995, pp. 746-753.
16. Iglesias, S., and Mason, W. H., "Optimum Spanloads Incorporating Wing Structural Weight," First AIAA Aircraft Technology, Integration, and Operations Forum, AIAA, Reston, VA, Oct. 2001, pp. 1-10; also AIAA Paper 2001-5234.
17. Grasmeyer, J. M., Naghshineh, A., Tetrault, P. A., Grossman, B., Haftka, R. T., Kapania, R. K., Mason, W. H., and Schetz, J. A., "Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft with Tip-mounted Engines," MAD Center Rept. MAD-98-01-01, Jan. 1998.
18. Giesing, J. P., and Wakayama, S., "A Simple Cost Related Objective Function for MDO of Transport Aircraft," 35th Aerospace Sciences Meeting and Exhibit, AIAA, Reston, VA, Jan. 1997, pp. 1-14; also AIAA Paper 97-0356.
19. Johnson, V. S., "Minimizing Life Cycle Cost for Subsonic Commercial Aircraft," Journal of Aircraft, Vol. 27, No. 2, Feb. 1990, pp. 139-145.
20. Samareh, J. A., "Aerodynamic Shape Optimization Based on FreeForm Deformation," 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA, Reston, VA 30 Aug.-l Sept. 2004.
21. Jameson, A., Shankaran, S., Martinelli, L., Haimes, B., "Aerodynamic Shape Optimization of Complete Aircraft Configurations Using Unstructured Grids," 42ndAerospace Science Meeting, AIAA, Reston, VA, 2004, pp. 1-14; also AIAA Paper 2004-0533.
22. Martins, J. R., Alonso, J., and Reuther, J., "A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design," Optimization and Engineering, Vol. 6, No. 1, March 2005, pp. 33-62.
23. Chiba, K., Gbayashi, S., Nakahashi, K., and Morino, H., "High-Fidelity Multidisciplinary Design Optimization of Aerostructural Wing Shape for Regional Jet," AIAA Paper 2005-5080, June 2005.
24. Obayashi, S., Pyama, A., and Nakamura, T., 'Transonic Wing Shape Optimization Based on Evolutionary Algorithms," High Performance Computing, Third International Symposium, ISHPC 2000, edited by M. Valero, K. Joe, M. Kitsuregawa, and H. Tanaka, Springer-Verlag, Berlin, Pet. 2000.
25. Isikveren, A., "Parametric Modeling Techniques in Industrial Conceptual Transport Aircraft Design," SAE Paper 2003-01-3052, Sept. 2003.
26. General Aviation Synthesis Program-GASP, NASA CR-152303, Cosmic Program ARC-11434, 1978.
27. Abdo, M., Piperni, P., Isikveren, A., and Kafyeke, F., "Optimization of a Business Jet," Canadian Aeronautics and Space Institute Annual General Meeting, Aircraft Design & Development Symposium, [CDROM], Canadian Aeronautics and Space Institute, Ottawa, Toronto, April 2005.
28. Abdo, M., L'Heureux, R., Pépin, F., and Kafyeke, F., "Equivalent Finite Element Wing Structural Models Used for AerodynamicsStructures Interaction," CASI 16th Aerospace Structures & Materials Symposium, [CD-ROM], Canadian Aeronautics and Space Institute, Ottawa, Toronto, 2003.
29. Chintapalli, S., Sedaghati, R., Li, J., and Abdo, M., "Minimum Mass Design of Stringer Stiffened Compression Panels Under Compressive Axial Load," WCSMO6 Paper 2005-1671, May 2005.
30. Reymond, M., and Miller, M., MSC/NASTRAN, Quick Reference Guide, Ver. 68, 1994.
31. [31 ] Kafyeke, F., and Piperni, P., "Applications of KTRAN Transonic Small Disturbance Code to the Challenger Business Jet Configuration with Winglets," SAE Paper 881483, Oct. 1988.
32. Piperni, P., and Kafyeke, F., "Applications of the KTRAN Transonic Small Disturbance Code to the Complete CF-18 Aircraft with Stores," Canadian Aeronautics and Space Institute (CASI) Journal, Vol. 36, No. 3, Sept. 1990, pp. 153-165.
33. Piperni, P., Patel, K., and Kafyeke, F., "The Prediction of Aircraft Trim Drag in Transonic Flight Using CFD," 46th Annual CASI Conference, Montreal, [CD-ROM], Canadian Aeronautics and Space Institute, Ottawa, May 1999.
34. Hoerner, S. F., Fluid Dynamic Drag, Hoerner Fluid Dynamics, Brick Town, NJ, 1965.
35. Lock, R. C., "Prediction of the Drag of Wings at Subsonic Speeds by Viscous/Inviscid Interaction Techniques," AGARD Rept. 723, 1985.
36. Munk, M., "The Minimum Induced Drag of Airfoils," NACA, Rept. 121, 1921.
37. Kuhn, P., Peterson, J., and Levin, L., "A Summary of Diagonal Tension, Part 1-Methods of Analysis," NACA Technical Note 2661, 952.
38. Burt, M. E., "Weight Prediction for Wings of Box Construction," RAE Report No. Structures 186, 1955.
39. Shanley, F. R., Weight-Strength Analysis of Aircraft Structures, Dover Publications Inc., New York, 1960.
40. Farrar, D. J., "The Design of Compression Structures for Minimum Weight," Journal of the Royal Aeronautical Society, Vol. 2, Nov. 1949, pp.1041-1052.
41. Isikveren, A., "Identifying Economically Optimum Flight Techniques of Transport Aircraft," Journal of Aircraft, Vol. 39, No. 4, JulyAug. 2002, pp. 528-544.
42. Torenbeek, E., Synthesis of Subsonic Airplane Design, Kluwer Academic Publication, Norwell, MA, 1988.
43. Torenbeek, E., "Optimum Cruise Performance of Subsonic Transport Aircraft," Delft University of Technology, Rept. LR-787, Faculty of Aerospace Engineering, The Netherlands, March 1995.