Application of a Hinge-Moment-Based Envelope Protection System on a Wing-Reference-Cited by-同舟云学术

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Application of a Hinge-Moment-Based Envelope Protection System on a Wing

Published:2014-11 Issue:6 Volume:51 Page:2038-2042
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ansell Phillip J.¹,Kerho Michael F.²,Bragg Michael B.³

Affiliation:

1. Department of Aerospace Engineering, University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

2. Rolling Hills Research Corporation, El Segundo, California 90245

3. Dean of the College of Engineering, University of Washington, University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032703

Reference8 articles.

1. Aerodynamic Simulation of a Horn-Ice Accretion on a Subscale Model

2. WickensR. H.NguyenV. D. “Wind Tunnel Investigation of a Wing-Propeller Model Performance Degradation due to Distributed Upper-Surface Roughness and Leading Edge Shape Modification,” AGARD CP-496, Paper 11, 1991.

3. Heavy rain influence on airplane accidents

4. Effect of Airfoil Geometry on Performance with Simulated Intercycle Ice Accretions

5. Sensing Aircraft Icing Effects by Unsteady Flap Hinge-Moment Measurement

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