Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle-Reference-Cited by-同舟云学术

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Numerical investigation of short takeoff and landing exhaust system using bypass dual throat nozzle

Published:2023-07 Issue: Volume:138 Page:108316
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Yuqi^ORCID,Xu Jinglei,Pan Ruifeng,Li Yao,Ma Zhao,Huang Shuai

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference53 articles.

1. Future systems;Ciminera,2013

2. History of the Pegasus vectored thrust engine;Hooker;J. Aircr.,1981

3. A review of lift nozzle model testing at Rolls-Royce;Eames,1993

4. F-35 air vehicle technology overview;Wiegand,2019

5. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs;Ducard;Aerosp. Sci. Technol.,2021

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

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

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

3. Effect of Bypass Duct on the Thrust Vectoring Performance of Dual Throat Nozzle in a Supersonic Aircraft;Journal of Fluids Engineering;2024-02-28

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