Icing Analysis of the NASA S3 Icing Research Aircraft Using LEWICE3D Version 2

2007-01-3324

9/24/2007

Authors
Abstract
Content
Results of an icing analysis of the NASA S3 Icing Research Aircraft will be presented along with the latest improvements to the LEWICE3D ice accretion program. The icing results include collection efficiency and ice shape calculations for the S3. Recent improvements to the roughness and ice density models, performance and accuracy of the overall collection efficiency algorithm, and to the user interface for the LEWICE3D program will be discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/2007-01-3324
Citation
Bidwell, C., "Icing Analysis of the NASA S3 Icing Research Aircraft Using LEWICE3D Version 2," 2007 SAE Aircraft and Engine Icing International Conference, Seville, Spain, September 24, 2007, https://doi.org/10.4271/2007-01-3324.
Additional Details
Publisher
Published
9/24/2007
Product Code
2007-01-3324
Content Type
Technical Paper
Language
English