Multiobjective Performance Optimization of a Coaxial Compound Rotorcraft Configuration-Reference-Cited by-同舟云学术

Multiobjective Performance Optimization of a Coaxial Compound Rotorcraft Configuration

Published:2017-07 Issue:4 Volume:54 Page:1498-1507
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hersey Sean¹,Sridharan Ananth¹,Celi Roberto¹

Affiliation:

1. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033999

Reference19 articles.

1. Recent Applications of Design Optimization to Rotorcraft-A Survey

2. A Survey of Recent Developments in Rotorcraft Design Optimization

3. OrrS. A.NarducciR. P. “Framework for Multidisciplinary Analysis, Design, and Optimization with High-Fidelity Analysis Tools,” NASA CR-2009-215563, Feb. 2009.

4. Aeromechanics Analysis of a Heavy Lift Slowed-Rotor Compound Helicopter

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