Development of Theoretical Method for Two-Dimensional Multi-Element Airfoil Analysis and Design. Part II: Leading-Edge Slat Design Method.

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Report Number: AFFDL TR 72-96 Part 2
Author(s): McGregor, O. Wayne, McWhirter, Jack W.
Corporate Author(s): General Dynamics Fort Worth Tex Convair Aerospace Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1972-08
Pages: 176
Contract: F33615-71-C-1597
DoD Project: 1366
Identifier: AD0749485

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Provenance: Lockheed Martin Missiles & Fire Control

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