An Intelligent Algorithm for Aerodynamic Parameters Calibration of Wind Tunnel Experiment at a High Angle of Attack
In this paper, an intelligent algorithm for the aerodynamic parameter calibration of wind tunnel experiments of advanced layout aircraft at a high angle of attack is proposed. The proposed algorithm is based on a homologous comparison and tuning algorithm, and it can effectively improve the accuracy...
Saved in:
| Main Authors: | Yeguang Wang, Shitong Jian, Zhigang Wang, Rui Fan, Peng Han, Yongxi Lyu |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2023-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2023/3093526 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Parameter Identification and Control Method of a Hypersonic Wind Tunnel Attack Angle Mechanism
by: Guoliang Zheng, et al.
Published: (2020-10-01) -
The effect of Flow Speed and Angle of Attack on the Aerodynamic Noise of NACA 0012 Airfoil
by: Hussein Mohammad, et al.
Published: (2023-12-01) -
AERODYNAMIC CHARACTERISTICS OF “FAN-IN-FIN” SYSTEM IN CONDITION OF FLOWING UNDER ZERO ATTACK ANGLE
by: V. I. Shaydakov
Published: (2016-11-01) -
Aerodynamic Test of AGARD-B Model at Mach 10 in Arc-heated High-Enthalpy Wind Tunnel
by: Tingting ZHANG, et al.
Published: (2024-09-01) -
Wind Tunnel Test Investigation on Unsteady Aerodynamic Coefficients of Iced 4-Bundle Conductors
by: Mengqi Cai, et al.
Published: (2019-01-01)