A method for flexible design integration

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 1899-1907

  Stettner, Martin ^a   Mavris, Dimitri N ^b   Schrage, Daniel P ^b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSERVOELASTICITY; DESIGN; FIGHTER AIRCRAFT; OPTIMIZATION; STRUCTURAL DYNAMICS; AIRCRAFT; COMPUTER SIMULATION; PERFORMANCE; RAPID PROTOTYPING; SCHEDULING;

CONTRIBUTING ANALYSIS; DESIGN ENVIRONMENT; DESIGN SIMULATIONS; LARGE-SCALE OPTIMIZATION; LEVEL OF ABSTRACTION; MULTIPLE DECOMPOSITION; SPECIFIC INFORMATION; TILT-ROTOR AIRCRAFTS;

STRUCTURAL DESIGN; AEROSPACE ENGINEERING;

DESIGN SIMULATION MODEL; TILTROTOR AIRCRAFT AERO;

EID: 0029722756     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1540     Document Type: Conference Paper

References (21)

1. Sobieszczanski-Sobieski, J., “On the Sensitivity of Complex Internally Coupled Systems,” NASA TM 100537, January 1988.
2. Rogers, J.L., “DeMAID - A Design Manager’s Aide for Intelligent Decomposition User’s Guide,” NASA TM 101575, March 1989.
3. Bloebaum, C.L., Hajela, P., and Sobieszczanski-Sobieski, J., “Non-Hierarchic Decomposition in Structural Optimization,” Third Air Force / NASA Symposium on Recent Advances in Multidisciplinary Analysis and Optimization, San Francisco, CA, September 1990.
4. Dovi, A.R., Wrenn, G.A., Barthelemy, J.-F. M., Coen, P.O., and Hall, L.E., “Multidisciplinary Design Integration System For a Supersonic Transport Aircraft,” Fourth AIAA/USAF/NASA/ OAI Symposium on Multidisciplinary Analysis and Optimization, Cleveland, OH, September 1992.
5. Townsend, J.C., Weston, R.P., and Eidson, T.M., “A Programming Environment for Distributed Complex Computing - An Overview of the Framework for Interdisciplinary Optimization (FIDO) Project,” NASA-TM- 109058, December 1993.
6. Jones, K.H., Randall, D.P., and Cronin, C.K., “Information Management for a large Multidisciplinary Project,” Fourth AIAA/USAF/ NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, Cleveland, OH, September 1992.
7. Bloebaum, C.L., “An Intelligent Decomposition Approach for Coupled Engineering Systems,” Fourth AIAA/USAF/NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, Cleveland, OH, September 1992.
8. Kroo, I., and Takai, M., “A Quasi - Procedural, Knowledge - Based System for Aircraft Design,” AIAA/AHS/ASEE Aircraft Design, Systems and Operations Meeting, Atlanta, GA, September 1988.
9. Stevens, E., “LEGEND: Laboratory Environment for the Generation, Evaluation, and Navigation of Design,” Ph.D. Thesis, School of Aerospace Engineering, Georgia Institute of Technology, September 1993.
10. Sobieszczanski-Sobieski, J., “A Linear Decomposition Method for Large Optimization Problems - Blueprint for Development,” NASA TM 83248, February 1982.
11. Sobieszczanski-Sobieski, J., “Optimization by Decomposition: A Step from Hierarchic to Non- Hierarchic Systems,” Second NASA / Air Force Symposium on Recent Advances in Multidisciplinary Optimization, Hampton, VA, September 1988.
12. Renaud, J.E., Sellar, R.S., Batill, S.M., and Kar, P., “Design Driven Coordination Procedure for Concurrent Subspace Optimization in MDO,” 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Hilton Head, SC, April 1994.
13. Sobieski, I., and Kroo, I., “Collaborative Optimization Applied to an Aircraft Design Problem,” 34th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1996.
14. Balling, R.J., and Sobieszczanski-Sobieski, J., “Optimization of Coupled Systems: A Critical Overview of Approaches,” Fifth AIAA/NASA/ USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, September 1994.
15. Stettner, M., Mavris, D.N., and Schrage, D.P., “Aeroelastic Tailoring of a Civil Tiltrotor Configuration,” American Helicopter Society Vertical Lift Aircraft Design Conference, San Francisco, CA, January 1995.
16. Bloebaum, C.L., “An Intelligent Decomposition Approach for Coupled Engineering Systems,” Fourth AIAA/USAF/NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, Cleveland, OH, September 1992.
17. Studebaker, K., and Matuska, D., “Variable Diameter Tiltrotor Wind Tunnel Test Results,” 49th Annual Forum of the American Helicopter Society, St. Louis, MO, May 1993.
18. Schoen, A.H., Rosenstein, H., Stanzione, K., and Wisniewski, J.S., “User’s Manual for VASCOMP II, The V/STOL Aircraft Sizing and Performance Computer Program,” Boeing Vertol Company Report D8-0375, Vol. VI, Third Revision, May 1980.
19. Giles, G.L., “Further Generalization of an Equivalent Plate Representation for Aircraft Structural Analysis,” Journal of Aircraft, Vol. 26, No. 1, p. 67-74, January 1989.
20. Kvatemik, R.G., “Studies in. Tiltrotor VTOL Aircraft Aeroelasticity,” Doctoral Dissertation, Department of Solid Mechanics, Case Western Reserve, June 1973.
21. Stettner, M., “Tiltrotor Multidisciplinary Optimization,” Ph.D. Thesis, School of Aerospace Engineering, Georgia Institute of Technology, August 1995.