Effects of Bend–Twist Coupling on Composite Propeller Performance-Reference-Cited by-同舟云学术

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Effects of Bend–Twist Coupling on Composite Propeller Performance

Published:2000-10 Issue:4 Volume:7 Page:383-401
ISSN:1075-9417
Container-title:Mechanics of Composite Materials and Structures
language:en
Short-container-title:Mechanics of Composite Materials and Structures

Author:

M. Khan, Daniel O. Adams, Vinay Day Abdul¹²³

Affiliation:

1. a Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Science and Technology, Pakistan

2. b Department of Mechanical Engineering, University of Utah, Salt Lake City, Utah, USA

3. c Department of Aerospace Engineering and Engineering Mechanics, Iowa State University, Ames, Iowa, USA

Publisher

Informa UK Limited

Subject

Ceramics and Composites

Link

https://www.tandfonline.com/doi/pdf/10.1080/10759410050201717

Reference3 articles.

1. F. E. Weick, Full Scale Wind Tunnel Tests with a Series of Propellers of Different Diameters on a Single Fuselage, NACA Rep. 339, 1930.

2. F. E. Weick, Full Scale Wind Tunnel Tests on Several Metal Propellers Having Different Blade Forms, NACA Rep. 340, 1930.

3. W. J. Dwyer and J. B. Rogers, Aeroelastically Tailored Propellers, SAE Paper 770455, March 1977.

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