Zobrazeno 1 - 10
of 147
pro vyhledávání: '"Michael B. Bragg"'
Publikováno v:
Journal of Aircraft. 57:342-359
A comparison of computational and experimental ice accretions generated on three swept-wing models in the NASA Glenn Icing Research Tunnel is presented. The wind tunnel models span floor to ceiling...
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
Journal of Aircraft. 56:730-746
Hybrid-wing models are those that present the same leading-edge geometry of the full-scale aircraft wing and a redesigned aft section of reduced chord, such that models can be tested inside an icin...
Publikováno v:
Journal of Aircraft. 56:137-149
The certification of modern commercial aircraft requires manufacturers to demonstrate flight safety under various scenarios, including icing conditions. Although computational tools play a key role...
Publikováno v:
AIAA AVIATION 2020 FORUM.
Publikováno v:
AIAA AVIATION 2020 FORUM.
Publikováno v:
AIAA AVIATION 2020 FORUM.
Autor:
Brian S. Woodard, Michael B. Bragg
Publikováno v:
AIAA AVIATION 2020 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:
Michael B. Bragg, Phillip J. Ansell
Publikováno v:
Journal of Aircraft. 53:475-486
An experimental investigation was conducted on an NACA 0012 airfoil with a leading-edge horn-ice shape to identify and characterize flowfield unsteadiness related to ice-induced flow separation. This type of iced-airfoil flowfield was dominated by a