Finite Wing Lift-Curve Slope Calculations Using Lifting-Line Theory-Reference-Cited by-同舟云学术

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Finite Wing Lift-Curve Slope Calculations Using Lifting-Line Theory

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Bridges David¹

Affiliation:

1. Mississippi State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4839

Reference7 articles.

1. 1Prandtl,L."ApplicationsofModernHydrodynamicstoAeronautics,"NACAReportNo.116,1923.

2. 2Anderson,J.D.,FundamentalsofAerodynamics,3rded.,NewYork,McGraw-Hill,2001.

3. 3Glauert,H.,TheElementsofAerofoilandAirscrewTheory,Cambridge,England,CambridgeUniversityPress,1926.

4. 5McCormick,B.W.,Aerodynamics,AeronauticsandFlightMechanics,2nded.,NewYork,Wiley,1995.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Simultaneously Deriving Wing Twist and Planform from Two Lift Distributions;Journal of Aircraft;2020-05

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