Robust Design Optimization of Airfoils with Respect to Ice Accretion-Reference-Cited by-同舟云学术

Robust Design Optimization of Airfoils with Respect to Ice Accretion

Published:2011-01 Issue:1 Volume:48 Page:287-304
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ghisu Tiziano¹,Jarrett Jerome P.¹,Parks Geoffrey T.¹

Affiliation:

1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031100

Reference55 articles.

1. Wing Loading, Icing and Associated Aspects of Modern Transport Design

2. "Search for Answers Begins in Buffalo Plane Crash, CNN website, http://www.cnn.com/2009/US/02/13/plane.crash.new.york/index.html [retrieved 13 Feb. 2009].

3. Current Methods Modeling and Simulating Icing Effects on Aircraft Performance, Stability, Control

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