Effect of Aspect Ratio on Flow Through Serpentine Nozzles-Reference-Cited by-同舟云学术

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Effect of Aspect Ratio on Flow Through Serpentine Nozzles

Published:2012-05 Issue:3 Volume:49 Page:836-851
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Reynolds T.¹,Reeder M. F.¹

Affiliation:

1. Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031444

Reference18 articles.

1. Study of the compressible flow in a diffusing S-duct

2. Experimental and Numerical Investigation of Active Control of Inlet Ducts

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. Numerical Investigation of Local Adverse Pressure Gradient in Shape Changing Nozzles;AIAA SCITECH 2024 Forum;2024-01-04

2. The influence of the adverse pressure gradient on the flow characteristics of a serpentine nozzle with film cooling;Aerospace Science and Technology;2023-05

3. Comprehensive optimization design of aerodynamic and electromagnetic scattering characteristics of serpentine nozzle;Chinese Journal of Aeronautics;2021-03

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