A Unit Solution for the Load Distribution of a Nonrigid Wing by Matrix Methods-Reference-Cited by-同舟云学术

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A Unit Solution for the Load Distribution of a Nonrigid Wing by Matrix Methods

Published:1949-08 Issue:8 Volume:16 Page:470-476
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

PINES SAMUEL¹

Affiliation:

1. Republic Aviation Corporation,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.11835

Reference5 articles.

1. Matrix Development of Multhopp's Equations for Spanwise Air-Load Distribution

2. Frazer, Duncan, and Collar, Elementary Matrices; The MacMillan Company, New York, 1947.

3. Von Mises, R., Theory of Flight, pp.231-244; McGraw-Hill Book Company, Inc., New York.

Cited by 3 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. Statische aeroelastische Probleme;Grundlagen der Aeroelastik;1974

2. A Steady-Flow Aeroelastic Study by Electrical Analogy;Journal of the Aeronautical Sciences;1953-10

3. Equations for the Loading on Triangular Wings Having Supersonic Leading and Trailing Edges Due to Various Basic Twist Distributions;Journal of the Aeronautical Sciences;1953-07

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