UH-60A Rotor Analysis with an Accurate Dual-Formulation Hybrid Aeroelastic Methodology-Reference-Cited by-同舟云学术

UH-60A Rotor Analysis with an Accurate Dual-Formulation Hybrid Aeroelastic Methodology

Published:2020-01 Issue:1 Volume:57 Page:113-127
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Wilbur Isaac C.¹,Moushegian Alex¹,Smith Marilyn J.¹,Whitehouse Glen R.²

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150

2. Continuum Dynamics, Inc., Ewing, New Jersey 08618-2302

Funder

Armament Research, Development and Engineering Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035467

Reference29 articles.

1. Hover Performance Assessment of Several Tip Shapes using OVERFLOW

2. OVERTURNS Simulation of S-76 Rotor in Hover

3. Analysis of a Rotor in Hover using Hybrid Methodology

4. NicholsR. H.BuningP. G. User’s Manual for OVERFLOW, Version 2.2, NASA Langley Research Center, Hampton, VA, May 2014, https://overflow.larc.nasa.gov/home/users-manual-for-overflow-2-2/ [accessed 17 Dec. 2019]

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