Comparison of Ice Shapes on Full-Chord and Truncated Swept Wing Models-Reference-Cited by-同舟云学术

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Comparison of Ice Shapes on Full-Chord and Truncated Swept Wing Models

Published:2021-07-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2021 FORUM
language:
Short-container-title:

Author:

Lee Sam¹,Broeren Andy P.²,Potapczuk Mark G.²

Affiliation:

1. HX5, LLC

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2679

Reference17 articles.

1. Development of a Common Research Model for Applied CFD Validation Studies

2. A hybrid airfoil design method to simulate full-scale ice accretion throughout a given C(l)-range

3. Fujiwara, G.E.C., Design of 3D Swept Wing Hybrid Models for Icing Wind Tunnel Tests. M.S. Thesis,Univ. of Illinois, 2014.

Cited by 1 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. GlennICE 2.1 Capabilities and Results;AIAA AVIATION 2022 Forum;2022-06-20

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