Nonlinear Generalized Lifting-Line Coupling Algorithms for Pre/Poststall Flows-Reference-Cited by-同舟云学术

Nonlinear Generalized Lifting-Line Coupling Algorithms for Pre/Poststall Flows

Published:2015-07 Issue:7 Volume:53 Page:1784-1792
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gallay S.¹,Laurendeau E.¹

Affiliation:

1. Department of Mechanical Engineering, École Polytechnique de Montréal, Montréal, Québec H3C 3A7, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053530

Reference19 articles.

1. Maximum lift prediction for multielement wings

2. CebeciT.ShaoJ.KafyekeF.LaurendeauE., Computational Fluid Dynamics for Engineers: From Panel to Navier–Stokes Methods with Computer Programs, Springer, New York, 2005, pp. 10–17.

3. HessJ. L.SmithA. “Calculation of Non-Lifting Potential Flow About Arbitrary Three-Dimensional Bodies,” Defense Technical Information Center TR, ES-40622, Fort Belvoir, VA, 1962.

4. Predicting Maximum Lift Coefficient for Twisted Wings Using Lifting-Line Theory

5. WeissingerJ. “The Lift Distribution of Swept-Back Wings,” NACA TR-1120, 1947.

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