Numerical investigation of scalloping effect on lobed nozzle flow features and thermal mixing performance-Reference-Cited by-同舟云学术

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Numerical investigation of scalloping effect on lobed nozzle flow features and thermal mixing performance

Published:2023-05 Issue: Volume:136 Page:108240
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hou Rui,Hong Yongjun

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Radar/infrared integrated stealth optimization design of helicopter engine intake and exhaust system;Zhou;Aerosp. Sci. Technol.,2019

2. M. Paszko, Infrared signature suppression systems in modern military helicopters, Prace Instytutu Lotnictwa, 2017.

3. Multidisciplinary analysis of a complete infrared suppression system;Bettini,2007

4. Progress in helicopter infrared signature suppression;Zhang;Chin. J. Aeronaut.,2014

5. Numerical investigation of flow mixture enhancement and infrared radiation shield by lobed forced mixer;Shan;Appl. Therm. Eng.,2009

Cited by 2 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. Multi-objective optimization of IRS device with scalloped lobed nozzle on flow features and thermal mixing performance;International Communications in Heat and Mass Transfer;2024-06

2. Quantitative analysis of enhanced mixing and combustion by lobed mixer in a ramjet engine: Study using hyperbolic Lagrangian coherent structures;Aerospace Science and Technology;2023-09

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