Title

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

Meeting Name

13th Congress of the International Council of the Aeronautical Sciences/AIAA Aircraft Systems and Technology Conference Proceedings

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.

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