Whirl Flutter Test of the Maryland Tiltrotor Rig: Overview-Reference-Cited by-同舟云学术

Whirl Flutter Test of the Maryland Tiltrotor Rig: Overview

Published:2022-01-03 Issue: Volume: Page:
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Container-title:AIAA SCITECH 2022 Forum
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Author:

Tsai Frederick¹,Sutherland James R.¹,Akinwale Akinola¹,Morin Amy¹,Gul Seyhan¹,Datta Anubhav¹

Affiliation:

1. University of Maryland at College Park A James Clark School of Engineering

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0567

Reference20 articles.

1. "Hover, Low Speed and Conversion Tests of a Tilt Rotor Aeroelastic Model," Tech. Rep. NASA CR-11»615, Bell Helicopter Company, V/STOLTilt Rotor Study, Vol.VI, May 197«.

2. Magee, J. P., and Alexander, H. R. "Wind Tunnel Tests of a Full Scale Hingeless Prop/Rotor Design for the Boeing Model 222 Tiltrotor Aircraft," Tech. Rep. D222-10059-1, Contract NAS2-6505, April 197«.

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. CR 1«7756, NASA, August 1975.

4. Ham, N. D., and Whitaker, H. P. "A Wind-Tunnel Investigation of Tilt-Rotor Gust Alleviation System," Tech. Rep. CR 15226», NASA, January 1978.

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