Design and experimental study of a bypass dual throat nozzle with the ability of short/vertical takeoff and landing-Reference-Cited by-同舟云学术

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Design and experimental study of a bypass dual throat nozzle with the ability of short/vertical takeoff and landing

Published:2022-02 Issue: Volume:121 Page:107301
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Huang Shuai,Xu Jinglei^ORCID,Yu Kaikai,Wang Yangsheng^ORCID,Pan Ruifeng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Lessons Learned in the Development of a National Cooperative Program;Walker,1997

2. Computational Investigation of the Aerodynamic Effects on Fluidic Thrust Vectoring;Deere,2000

3. Simulation of thrust control by fluidic injection and pintle in a solid rocket motor;Yan;Aerosp. Sci. Technol.,2020

4. Experimental research on vector control features of a pulse detonation tube with fluidic nozzle;Zhang;Aerosp. Sci. Technol.,2021

5. Fluidic thrust-vector control of supersonic jet using coflow injection;Heo;J. Propuls. Power,2012

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1. Analysis of mixing enhancement ability of bypass dual throat nozzle with single/multi-tabs;Heat Transfer Engineering;2024-07-03

2. Thrust vector V/STOL aircraft control based on angular acceleration estimation;Aerospace Science and Technology;2024-06

3. Aerodynamic Characteristics of the Novel Two-Dimensional Enhanced Shock Vector Nozzle;Aerospace;2024-05-07

4. Numerical investigation of dynamic characteristics of dual throat nozzle and bypass dual throat nozzle in thrust vectoring starting process;Chinese Journal of Aeronautics;2024-05

5. Dynamic characteristics and application of dual throat fluidic thrust vectoring nozzle;Chinese Journal of Aeronautics;2024-04

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