Aerodynamic Design of the DC-9 Wing and High-Lift System

670846

02/01/1967

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
The aerodynamic design and development of the wing and high lift system for the DC-9 family of short-to-medium range jet transports are reviewed.
Preliminary design methods used to establish major wing features such as area, sweep, average thickness, and taper are discussed as well as the more detailed design procedures.
Correlation of final flight test data on the Series 30 with early estimates show that, for the DC-9 wing and high lift system, the available methods resulted in a design that met all aerodynamic criteria established during the early design phase.
Meta TagsDetails
DOI
https://doi.org/10.4271/670846
Pages
12
Citation
Schaufele, R., and Ebeling, A., "Aerodynamic Design of the DC-9 Wing and High-Lift System," SAE Technical Paper 670846, 1967, https://doi.org/10.4271/670846.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670846
Content Type
Technical Paper
Language
English