Research of Comprehensive Modeling of Two-Dimensional Vector Nozzle/Actuator Load/Turbofan Engine-Reference-Cited by-同舟云学术

Research of Comprehensive Modeling of Two-Dimensional Vector Nozzle/Actuator Load/Turbofan Engine

Published:2023 Issue: Volume:11 Page:38708-38720
ISSN:2169-3536
Container-title:IEEE Access
language:
Short-container-title:IEEE Access

Author:

Wang Yuan¹,Jiang Wei²^ORCID,Zhang Haibo²^ORCID,Zheng Qiangang²^ORCID

Affiliation:

1. AECC Aero Engine Control System Institute, Wuxi, China

2. Energy and Power College, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

General Engineering,General Materials Science,General Computer Science,Electrical and Electronic Engineering

Link

http://xplorestaging.ieee.org/ielx7/6287639/10005208/10103607.pdf?arnumber=10103607

Reference27 articles.

1. Numerical study of shock/boundary layer interaction in supersonic overexpanded nozzles

2. Unsteady flow characteristics of dual-slots injection ports shock-induced thrust vectoring nozzle;jian-ming;Gas Turbine Experiment and Research,2021

3. A novel anomaly detection method for gas turbines using weight agnostic neural network search

4. Computational investigation on infrared radiation characteristic for two-dimensional vectoring nozzles with fluidic injection;kang;Proc Int Conf Transp Mech Electr Eng (TMEE),2011

5. Research on the aerodynamic and RCS characteristics of spherical convergent flap nozzle;xiao;Gas Turbine Experiment and Research,2021

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