Dual and Single Wing Design Integration-Optimized for Decalage Angle, R//E and M//C//R.

Author

K. Rokhsaz
B. P. Selberg, Missouri University of Science and TechnologyFollow

Recommended Citation

K. Rokhsaz and B. P. Selberg, "Dual and Single Wing Design Integration-Optimized for Decalage Angle, R//E and M//C//R.," Fluid Dynamics and Co-located Conferences, American Institute of Aeronautics and Astronautics (AIAA), Jan 1984.

The definitive version is available at https://doi.org/10.2514/6.1984-2161

Meeting Name

2nd Applied Aerodynamics Conference

Department(s)

Mechanical and Aerospace Engineering

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1984 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.

Publication Date

01 Jan 1984