Cooperation of Trailing-Edge Flap and Shock Control Bump for Robust Buffet Control and Drag Reduction
At transonic flight conditions, the buffet caused by the interaction between the shock waves and the boundary layers can degrade an aircraft’s aerodynamic performance and even threaten its safety. In this paper, the shock control bumps, originally designed to reduce the wave drag at cruise speeds, a...
Main Authors: | Shenghua Zhang, Feng Deng, Ning Qin |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-10-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/9/11/657 |
Similar Items
-
Closed-Loop Control of Transonic Buffet Using Active Shock Control Bump
by: Feng Deng, et al.
Published: (2023-06-01) -
Unsteady Simulation of Transonic Buffet of a Supercritical Airfoil with Shock Control Bump
by: Yufei Zhang, et al.
Published: (2021-07-01) -
A Numerical Investigation of the Geometric Parametrisation of Shock Control Bumps for Transonic Shock Oscillation Control
by: Jack A. Geoghegan, et al.
Published: (2020-04-01) -
Transonic Buffet Active Control with Local Smart Skin
by: Kai Ren, et al.
Published: (2022-06-01) -
Passive Transonic Shock Control on Bump Flow for Wing Buffet Suppression
by: Davide Di Pasquale, et al.
Published: (2023-06-01)