Experimental and numerical investigation on design parameters of slot nozzles-Reference-Cited by-同舟云学术

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Experimental and numerical investigation on design parameters of slot nozzles

Published:2023-10 Issue: Volume:141 Page:108509
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yu Haixu,Wei Zhijun

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference34 articles.

1. Supersonic flow separation with application to rocket engine nozzles;Östlund;Appl. Mech. Rev.,2005

2. Nozzle flow separation;Hadjadj;Shock Waves,2009

3. Numerical study of restricted shock separation in a compressed truncated perfect nozzle;Shimizu;AIAA J.,2006

4. Origin of side-loads in a subscale truncated ideal contour nozzle;Verma;Aerosp. Sci. Technol.,2017

5. Advanced rocket nozzles;Hagemann;J. Propuls. Power,1998

Cited by 1 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. Evaluation of Passively Cooled Variable Area Ratio Nozzle Design;AIAA SCITECH 2024 Forum;2024-01-04

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