Title

Aerodynamic-Structural Study of Canard Wing, Dual Wing, and Conventional Wing Systems for General Aviation Applications

Abstract

An analytical aerodynamic-structural airplane configuration study was conducted to assess performance gains achievable through advanced design concepts. The mission specification was for 350 mph, range of 1500 st. mi., at altitudes between 30,000 and 40,0

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Aerodynamic Characteristics; Aerodynamic Configurations; Aircraft Design; Canard Configurations; General Aviation Aircraft; Structural Analysis; Weight Analysis; Wings

Document Type

Report - Technical

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1985 University of Missouri--Rolla, All rights reserved.

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