Laminar-Turbulent Transition in Swept-Wing Flows with a Supercritical Forward-Facing Step
More Info
expand_more
expand_more
Abstract
Achieving and maintaining laminar flow on large swept lifting surfaces of subsonic aircraft poses a considerable challenge.
Files
978_3_031_47028_8_23.pdf
(pdf | 0.882 Mb)
- Embargo expired in 03-06-2024
License info not available