Zobrazeno 1 - 10
of 51
pro vyhledávání: '"Mark G. Potapczuk"'
Publikováno v:
Journal of Aircraft. 58:894-906
Icing on three-dimensional lifting surfaces has been shown to produce highly complex flowfields. However, there is a lack of experimental and computational information in the public domain regardin...
Publikováno v:
AIAA AVIATION 2022 Forum.
Autor:
Jen-Ching Tsao, Mark G. Potapczuk
Publikováno v:
AIAA AVIATION 2022 Forum.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Autor:
Michael B. Bragg, Mark G. Potapczuk, Brian S. Woodard, Sam Lee, Timothy G. Smith, Andy P. Broeren
Publikováno v:
SAE Technical Paper Series.
Understanding the aerodynamic impact of swept-wing ice accretions is a crucial component of the design of modern aircraft. Computer-simulation tools are commonly used to approximate ice shapes, so the necessary level of detail or fidelity of those si
Autor:
Jen-Ching Tsao, Mark G. Potapczuk
Publikováno v:
SAE Technical Paper Series.
An ice shape database has been created to document ice accretions on a 21-inch chord NACA0012 model and a 72-inch chord NACA 23012 airfoil model resulting from an exposure to a Supercooled Large Drop (SLD) icing cloud with a bimodal drop size distrib
Publikováno v:
Progress in Aerospace Sciences. 111:100583
Extensive experimental studies and associated reviews have been conducted to better understand the aerodynamic impact of iced lifting surfaces based on measurements. This review is a computational compliment to these previous studies to understand ho
Publikováno v:
2018 Atmospheric and Space Environments Conference.
A computational icing risk analysis utilizing LEWICE3D was performed for the D8 Double Bubble aircraft. A variety of discrete drop sizes spanning the Appendix C and O regimes were simulated. For computational efficiency a 50-bin global discretization
Autor:
Jen-Ching Tsao, Mark G. Potapczuk
Publikováno v:
2018 Atmospheric and Space Environments Conference.
An ice shape database has been created to document ice accretions on a 72-inch chord NACA 23012 airfoil model resulting from an exposure to a Supercooled Large Drop (SLD) icing cloud with a bimodal drop size distribution. The ice shapes created were