Dual Wing, Swept Forward Swept Rearward Wing, and Single Wing Design Optimization for High Performance Business Airplanes

Author

M. D. Rhodes
B. P. Selberg, Missouri University of Science and TechnologyFollow

Recommended Citation

M. D. Rhodes and B. P. Selberg, "Dual Wing, Swept Forward Swept Rearward Wing, and Single Wing Design Optimization for High Performance Business Airplanes," Proceedings of the 13th Congress of the International Council of the Aeronautical Sciences/AIAA Aircraft Systems and Technology Conference (1982, Seattle, WA), American Institute of Aeronautics and Astronautics (AIAA), Aug 1982.

Meeting Name

13th Congress of the International Council of the Aeronautical Sciences/AIAA Aircraft Systems and Technology Conference (1982: Aug. 22-27, Seattle, WA)

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Aerodynamic Behavior; Closely Coupled Dual Wing; Minimum Cruise Drag; Multiple Wing System Aircraft; Optimum Multiple Wing Geometry; Single Wing Baseline Design

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1982 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.

Publication Date

27 Aug 1982