Fundamental Understanding and Prediction of Loads and Stability of a Full-scale Hingeless Tiltrotor-Reference-Cited by-同舟云学术

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Fundamental Understanding and Prediction of Loads and Stability of a Full-scale Hingeless Tiltrotor

Published:2021-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2021 Forum
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Author:

Gul Seyhan¹,Datta Anubhav¹

Affiliation:

1. University of Maryland, College Park

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. Johnson, W., Yamauchi, G. K., and Watts, M. E. “NASA Heavy Lift Rotorcraft Systems Investigation,” Tech. Rep. NASA/TP2005-213467, December 2005.

2. Magee, J. P., and Alexander, H. “Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model Volumes I-IV,” Tech. Rep. NASA-CR-151936, Boeing Vertol Company, September 1976.

3. Ham, N. D., Bauer, P. H., Lawrence, T. H., and Yasue, M. “A Study of Gust and Control Response of Model Rotor-Propellers in a Wind Tunnel Airstream,” Tech. Rep. NASA-CR-137756, August 1975.

4. Ham, N. D., and Whitaker, H. P. “A Wind-Tunnel Investivation of Tilt-Rotor Gust Alleviation Systems,” Tech. Rep. NASA-CR-152264, January 1978.

Cited by 1 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. Whirl Flutter Test of the Maryland Tiltrotor Rig: Prediction and Validation;AIAA SCITECH 2022 Forum;2022-01-03

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