Validations of Rotor Load Analysis Using Flexible Multibody Dynamics with Multiple Wake Panels for Low-Speed Flights-Reference-Cited by-同舟云学术

Validations of Rotor Load Analysis Using Flexible Multibody Dynamics with Multiple Wake Panels for Low-Speed Flights

Published:2018-08-18 Issue:4 Volume:19 Page:863-877
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Park Jae-Sang^ORCID

Funder

National Research Foundation of Korea

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/article/10.1007/s42405-018-0070-y/fulltext.html

Reference23 articles.

1. Bauchau OA (2006) DYMORE solutions: simulation tools for flexible multibody systems, http://www.dymoresolutions.com . Accessed 1 Mar 2018

2. Mantegazza P (2018) MBDYN: free multibody dynamics simulation. https://www.mbdyn.org/ . Accessed 1 Mar 2018

3. Peters DA, He CJ (1995) Finite state induced flow models part II: three-dimensional rotor disk. J Aircr 32(2):323–333

4. Liu H (2008) Interfacing comprehensive rotorcraft analysis with advanced aeromechanics and vortex wake models. Ph.D Thesis, School of Aerospace Engineering, Georgia Institute of Technology

5. Abras JN (2009) Enhancement of aeroelastic rotor airload prediction method. Ph.D Thesis, School of Aerospace Engineering, Georgia Institute of Technology

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