The role of constraints in the MDO of a cantilever and strut-B raced wing transonic commercial transport aircraft

SAE Technical Papers

Volumn , Issue , 2000, Pages

  Ko, A ^a   Grossman, B ^a   Mason, W H ^a   Haftka, R T ^b  

^a Virginia Polytechnic Institute and State University   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN AIDS; ENGINES; FUSELAGES; LAGRANGE MULTIPLIERS; NANOCANTILEVERS; NAVIGATION; STRUTS; TRANSPORT AIRCRAFT; VISUALIZATION;

COMMERCIAL TRANSPORT; DESIGN CONFIGURATIONS; DESIGN CONSTRAINTS; DESIGN SPACE VISUALIZATION; DESIGN VISUALIZATION; MULTIDISCIPLINARY DESIGN OPTIMIZATION; PASSENGER AIRCRAFTS; STRUT-BRACED WING;

SUPERSONIC AIRCRAFT;

EID: 85072451093     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2000-01-5609     Document Type: Conference Paper

References (31)

1. Pfenniger, W., "Design Considerations of Large Subsonic Long Range Transport Airplanes with Low Drag Boundary Layer Suction" Northrop Aircraft, Inc., Report NAI-58-529 (BLC-111), 1958. (Available from DTIC as AD 821 759)
2. Kulfan, R.M., and Vachal, J.D., "Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes" Boeing Commercial Airplane Company, AFFDL-TR-78-16, February 1978.
3. Park, P.H., "The Effect on Block Fuel Consumption in a Strutted vs. Cantilever Wing for a Short Haul Transport Including Strut Aerolastic Considerations" AIAA Paper 78-1454, 1978.
4. Turriziani, R.V., Lovell, W.A., Martin, G.L., Price, J.E., Swanson, E.E., And, Washburn, G.F., "Preliminary Desing Characteristics of a Subsonic Business Jet Concept Employing an Aspect Ratio 25 Strut-Braced Wing" NASA CR-159361, October 1980.
5. Grasmeyer, J.M., Naghshineh-Pour A.H., Tetrault, P.A., Grossman, B., Haftka, R.T., Kapania R.K., Mason, W.H., Schetz, J.A., "Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft with Tip-Mounted Engines" MAD Center Report 98-01-01, Virignia Tech, January 1998.
6. Grasmeyer, J.M., "Multidisciplinary Design Optimization of a Strut-Braced Wing Aircraft" MS Thesis, Virginia Polytechnic Institute & State University, April 1998A.
7. Martin, K.C., and Kopec, B.A., "A Structural and Aerodynamic Investigation of a Strut-Braced Wing Transport Aircraft Concept" Lockheed-Martin Aeronautical Systems, Marietta, GA, LG98ER0431, November 1998.
8. Gundlach, J.F., Tetrault, P.A., Gern, F.H., Nagshineh-Pour, A., Ko, A., Schetz, J.A., Mason, W.H., Kapania, R.K., and Grossman, B., " Multidisciplinary Design Optimization of a Strut-Braced Wing Transonic Transport" AIAA Paper 2000-0420, 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2000.
9. Naghshineh-Pour, A., "Structural Optimization and Design of a Strut-Braced Wing Aircraft" MS Thesis, Virginia Tech, November 1998.
10. Gern, F.H., Gundlach, J.F., Ko, A., Naghshineh-Pour, A., Sulaeman, E., Tetrault P.A., Grossman, B., Haftka, R.T., Kapania R.K., Mason, W.H., and Schetz, J.A., "Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing" SAE 1999-01-5621, 1999 World Aviation Congress, San Francisco, CA, Oct. 19-21, 1999.
11. Gern, F.H., Sulaeman, E., Naghshineh-Pour, A., Kapania, R.K., and Haftka, R.T., "Flexible Wing Model for Structural Wing Sizing and Multidisciplinary Design Optimization of a Strut-Braced Wing," AIAA Paper 2000-1427, 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Atlanta, GA, April 3-6, 2000.
12. Jensen, S.C., Rettie, I.H., and Barber, E.A., "Role of Figures of Merit in Design Optimization and Technology Assessment" Journal of Aircraft, Vol. 18, No. 2, February 1981, pp. 76-81. (Pubitemid 11495171)
13. Vanderplaats Research and Development, Inc., DOT User's Manual, Version 4.20, Colorado Springs, CO, 1995.
14. Gundlach, J.F., Naghshineh-Pour, A.H., Gern, F., Tetrault, P.A., Ko, A., Schetz, J.A., Mason, W.H., Kapania R.K., Grossman, B., Haftka, R.T., "Multidisciplinary Design Optimization and Industry Review of a 2010 Strut-Braced Wing Transonic Transport" MAD Center Report 99-06-03, 1999.
15. Braslow, A.L., Maddalon, D.V., Bartlett, D.W., Wagner, R.D., and Collier, F.S., "Applied Aspects of Laminar-Flow Technology" Viscous Drag Reduction in Boundary Layers, AIAA, Washington D.C., 1990. pp. 4778.
16. Grasmeyer, J.M., "A Discrete Vortex Method for Calculating the Minimum Induced Drag and Optimum Load Distribution for Aircraft Configurations with Noncoplanar Surfaces" VPI-AOE-242, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia, 24061, January 1998.
17. Mason, W.H., "Analytic Models for Technology Integration in Aircraft Design," AIAA-90-3262, September 1990.
18. Malone, B., and Mason, W.H., "Multidisciplinary Optimization in Aircraft Design Using Analytic Technology Models," Journal of Aircraft, Vol. 32, No. 2, March-April 1995, pp. 431-438.
19. Hoerner, S. F., Fluid-Dynamic Drag: Practical Information on Aerodynamic Drag and Hydrodynamic Resistance, pp. 8-1-8-20, published by, Hoerner S.F., Bakersfield, CA, 1965.
20. Tetrault, P.A., "Numerical Prediction of the Interference Drag of a Streamlined Strut Intersecting a Surface in Transonic Flow," Ph.D. dissertation, Virginia Polytechnic Institute & State University" 2000. (Available at http://etd.vt.edu)
21. Tetrault, P.A., Schetz, J.A., and Grossman, B., "Numerical Prediction of the Interference Drag of a Streamlined Strut Intersecting a Surface in Transonic Flow," AIAA Paper 2000-0509, 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 10-13, 2000.
22. Pirzadeh, S., "Structured Background Grids for Generation of Unstructured Grids by Advancing-Front Method" AIAA Journal, pp. 257-265, February 1993. (Pubitemid 23640426)
23. Frink, N. T., Parikh, P., and Pirzadeh, S., "A Fast Upwind Solver for the Euler Equations on Three-Dimensional Unstructured Meshes" AIAA Paper 910102, 1991.
24. Frink, N. T., Pirzadeh, S., and Parikh, P., "An Unstructured-Grid Software System for Solving Complex Aerodynamic Problems" NASA CP-3291, May 1995.
25. McCullers, L.A., FLOPS User's Guide, Release 5.81, NASA Langley Research Center.
26. Grasmeyer, J.M., "Stability and Control Derivative Estimation and Engine-Out Analysis," VPI-AOE-254, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061, 1998.
27. Mattingly, J.D., Heiser, W.H., and Daley, D.H., Aircraft Engine Design, AIAA, Washington, D.C., 1987.
28. Torenbeek, E., Synthesis of Subsonic Airplane Design, Delft University Press, Delft, The Netherlands, 1982.
29. Roskam, J., and Lan, C.-T. E., Airplane Aerodynamics and Performance, DARCorporation, Lawrence, KS, 1997.
30. Vanderplaats, G.N., Numerical Optimization Techniques for Engineering Design, Vanderplaats Research & Development, Inc., Colorado Springs, CO, pp. 16-22.
31. Ko, A., "The Role of Constraints and Vehicle Concepts in Transport Design: A Comparison of Cantilever and Strut-Braced Wing Airplane Concepts" MS Thesis, Virginia Polytechnic Institute & State University, April 2000.