Title

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

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.


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