Slowed Hingeless Rotor Wind Tunnel Tests and Validation at High Advance Ratios-Reference-Cited by-同舟云学术

Slowed Hingeless Rotor Wind Tunnel Tests and Validation at High Advance Ratios

Published:2021-01 Issue:1 Volume:58 Page:153-166
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wang Xing¹,Bauknecht André²,Maurya Shashank¹,Chopra Inderjit¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

2. Technical University of Braunschweig, 38106 Braunschweig, Germany

Funder

University of Maryland, Vertical Lift Research Center of Excellence

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference20 articles.

1. WheatleyJ. B.HoodM. J. “Full-Scale Wind Tunnel Tests of the PCA-2 Autogiro Rotor,” NACA TR-515, Jan. 1935. 10.1016/s0016-0032(35)90378-7

2. JenkinsJ. L. Jr, “Wind Tunnel Investigation of a Lifting Rotor Operating at Tip-Speed Ratios from 0.65 to 1.45,” NASA TN D-2628, Feb. 1965.

3. McCloudJ.BiggersJ.StroubR. H. “An Investigation of Full-Scale Helicopter Rotors at High Advance Ratios and Advancing Tip Mach Numbers,” NASA TN D-4632, July 1968.

4. CharlesB.TannerW. “Wind Tunnel Investigation of Semirigid Full-Scale Rotors Operating at High Advance Ratios,” United States Army Aviation Materiel Lab. TR 69-2, Jan. 1969.

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