@inproceedings{bd6d2c09728e4beea05b213c740d1243,
title = "Effect of ice shape fidelity on swept-wing aerodynamic performance",
abstract = "Low-Reynolds number testing was conducted at the 7 ft x 10 ft Walter H. Beech Memorial Wind Tunnel at Wichita State University to study the aerodynamic effects of ice shapes on a swept wing. A total of 17 ice shape configurations of varying geometric detail were tested. Simplified geometries of an ice shape may help improve current ice accretion simulation methods and therefore aircraft design, certification, and testing. For each configuration, surface pressure, force balance, and fluorescent mini-tuft data were collected and for a selected subset of configurations oil-flow visualization and wake survey data were collected. A comparison of two ice shape geometries and two configurations with simplified geometric detail for each ice shape geometry is presented in this paper.",
author = "Camello, {Stephanie C.} and Bragg, {Michael B.} and Broeren, {Andy P.} and Lum, {Christopher W.} and Woodard, {Brian S.} and Sam Lee",
note = "Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 9th AIAA Atmospheric and Space Environments Conference, 2017 ; Conference date: 05-06-2017 Through 09-06-2017",
year = "2017",
doi = "10.2514/6.2017-4373",
language = "English (US)",
isbn = "9781624104961",
series = "9th AIAA Atmospheric and Space Environments Conference, 2017",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "9th AIAA Atmospheric and Space Environments Conference, 2017",
}