A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests-Reference-Cited by-同舟云学术

A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:5th AIAA Atmospheric and Space Environments Conference
language:
Short-container-title:

Author:

Fujiwara Gustavo E. C.¹,Woodard Brian¹,Wiberg Brock¹,Mortonson Andrew J.¹,Bragg Michael¹

Affiliation:

1. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2826

Reference28 articles.

1. Iced-airfoil aerodynamics

2. 3Anderson,D.N."ManualofScalingMethods,"NASACR-2004-21287.

3. 4Von Glahn, U.H. "Use of Truncated Flapped Airfoils for Impingement and Icing Tests of Full-scale Leading-Edge Sections,"NACA/RM E56E11,1956.

4. Design of Subscale Airfoils with Full-Scale Leading Edges for Ice Accretion Testing

5. 6Mortonson, A. J. "Use of Hybrid Airfoil Design in Icing Wind Tunnel Tests of Large Scale Swept Wings," M.S. Dissertation, Dept.ofAerospace Engineering,UniversityofIllinoisat Urbana-Champaign, Champaign, IL,2011.

Cited by 22 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Scallop ice shape characteristics of swept wing based on large-scale icing wind tunnel experiment;Chinese Journal of Aeronautics;2023-12

2. A Parametric Design Method for Hybrid Airfoils for Icing Wind Tunnel Test;International Journal of Aerospace Engineering;2021-04-20

3. Effect of Spanwise Discontinuities on the Aerodynamics of a Swept Wing with Scalloped Ice Accretion;AIAA AVIATION 2020 FORUM;2020-06-08

4. Ice Shape Classification for Swept Wings;AIAA AVIATION 2020 FORUM;2020-06-08

5. Comparison of Computational and Experimental Ice Accretions of Large Swept Wings;Journal of Aircraft;2020-03