An Optimized Pressure-Based Method for Thrust Vectoring Angle Estimation
This research developed a pressure-based thrust vectoring angle estimation method for fluidic thrust vectoring nozzles. This method can accurately estimate the real-time in-flight thrust vectoring angle using only wall pressure information on the inner surface of the nozzle. We proposed an algorithm...
Main Authors: | Nanxing Shi, Yunsong Gu, Tingting Wu, Yuhang Zhou, Yi Wang, Shuai Deng |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-11-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/12/978 |
Similar Items
-
Numerical Investigation of Optimization of Injection Angle Effects on Fluidic Thrust Vectoring
by: F. Forghany, et al.
Published: (2017-01-01) -
Techniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review
by: Saadia Afridi, et al.
Published: (2023-07-01) -
Determination of Optimum Parameter Space of a Fluidic Thrust Vectoring System based on Coanda Effect Using Gradient-Based Optimization Technique
by: E. Kara, et al.
Published: (2023-07-01) -
Influence of Bypass Location on Two-Dimensional Shock Vectoring Nozzle
by: Bo-wen SHU, et al.
Published: (2023-09-01) -
Mathematical Modelling and Fluidic Thrust Vectoring Control of a Delta Wing UAV
by: Ahsan Tanveer, et al.
Published: (2023-06-01)