System design innovation using multidisciplinary optimization and simulation

8th Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2000, Pages

  Blair, Max ^a   Moorhouse, David ^a   Weisshaar, Terrence A ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Purdue University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894368538     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 03-06 April 2000 in Long Beach CA.
2. J. V. Zweber, M. Blair, G. Bharatram, H. Kamhawi, Structural and Manufacturing Analysis of a Wing Using the Adaptive Modeling Language, AIAA paper 98-1758 presented at the 39th AIAA/ ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 20-23 April 1998 in Long Beach CA.
3. M. Blair, S. Hill, T. A. Weisshaar, R. Taylor, Rapid Modeling with Innovative Structural Concepts, AIAA paper 98-1755 presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 20-23 April 1998 in Long Beach CA.
4. D. F. Veley, M. Blair, J. Zweber, "Aircraft Technology Assessment System, AIAA paper 98-4825, presented at the 7th AIAA/NASA/ISSMO Symposium on MultiDisciplinary Analysis and Optimization 2-4 September 1998 in St. Louis MO
5. J. Wolkovich., The Joined Wing: An Overview, Journal of Aircraft, Vol. 23, No. 3, 1986, pp. 161-178.
6. I. M. Kroo, J.W. Gallman, and S.C. Smith, Aerodynamic and Structural Studies of Joined-Wing Aircraft, Journal of Aircraft, Vol. 28, No. 1,1991, pp. 74-81.
7. J. W. Gallman, S. C. Smith, Optimization of Joined Wing Aircraft, Journal of Aircraft, Vol. 30, No. 6, Nov.-Dec. 1993, pp. 897-965.
8. J. W. Gallman and I. Kroo, Structural Optimization for Joined-Wing Synthesis, Journal of Aircraft, Vol. 33, No. 1, Jan.-Feb. 1996, pp. 214-223
9. H.-H. Lin, J.J. Jhou, and R. Stearman, Influence of Joint Fixity on the Aeroelastic Characteristics of a Joined Wing Structure, AIAA-90-0980-CP, 1990, pp. 1442-1454.
10. A. E. Magnus and M. E. Epton, PAN AIR-A Computer Program for Predicting Subsonic or Supersonic Linear Potential Flows About Arbitrary Configurations Using A Higher Order Panel Method, Vol I - Theory Document, NASA Contractor Report 3251.
11. V. B. Venkayya and V. A. Tischler, "Opstat-A Computer Program for the Optimal Design of Structures Subjected to Static Loads, Air Force Flight Dynamics Laboratory Technical Memorandum FBR-79-67, June 1979.