Accurate Predictions of Rotor Hover Performance at Low and High Disc Loadings-Reference-Cited by-同舟云学术

Accurate Predictions of Rotor Hover Performance at Low and High Disc Loadings

Published:2018-01 Issue:1 Volume:55 Page:89-110
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Jimenez Garcia A.¹,Barakos G. N.¹

Affiliation:

1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034144

Reference43 articles.

1. A review of helicopter rotor blade tip shapes

2. BalchD. T.SacculloA.SheehyT. W. “Experimental Study of Main Rotor/Tail Rotor/Airframe Interactions in Hover—Volume I,” NASA CR-166485, June 1983.

3. Experimental Study of Main Rotor/Tail Rotor/Airframe Interaction in Hover

4. BalchD. T.LombardiJ. “Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interactions in Hover. Vol. I—Text and Figures,” NASA CR–177336, Feb. 1985.

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