Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices-Reference-Cited by-同舟云学术

Efficient method for calculating the axial velocities induced along rotating blades by trailing helical vortices

Published:1984-06 Issue:6 Volume:21 Page:433-435
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Rand O.¹,Rosen A.¹

Affiliation:

1. Technion—Israel Institute of Technology, Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.44984

Reference6 articles.

1. Lerbs, H W An Approximate Theory of Heavily Loaded Free Running Propellers in the Optimum Condition Transactions of the Society of Naval Architects and Marine Engineers Vol 58 1950pp137183

2. Lerbs H W Moderately Loaded Propellers with a Finite Number of Blades and an Arbitrary Distribution of Circulation Transactions of The Society of Naval Architects and Marine Engineers Vol 60 1952 pp 73 123

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