Optimization process for configuration of flexible joined-wing

Authors

Cody C. Rasmussen, Air Force Institute of Technology
Robert A. Canfield, Air Force Institute of Technology
Maxwell Blair, Air Force Research Laboratory

Document Type

Article

Publication Date

1-2009

Abstract

Excerpt: An optimized configuration design utilizing both structural and aerodynamic analyses of a flexible joined-wing configuration is presented in this paper.

An optimized configuration design utilizing both structural and aerodynamic analyses of a flexible joined-wing configuration is presented in this paper.

Comments

Co-author C. Rasmussen was an AFIT PhD candidate at the time of this article. (AFIT-DS-ENP-10-J01, March 2009)

DOI

10.1007/s00158-008-0229-4

Source Publication

Structural and Multidisciplinary Optimization (ISSN 1615-147X | eISSN 1615-1488)

Recommended Citation

Rasmussen, C., Canfield, R. & Blair, M. Optimization process for configuration of flexible joined-wing. Struct Multidisc Optim 37, 265–277 (2009). https://doi.org/10.1007/s00158-008-0229-4