Performance Analysis of a Serpentine Inlet Design for an Unmanned Aerial Vehicle-Reference-Cited by-同舟云学术

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Performance Analysis of a Serpentine Inlet Design for an Unmanned Aerial Vehicle

Published:2021-07-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2021 FORUM
language:
Short-container-title:

Author:

Brandon Jacob A.¹,Whitfield Clifford A.¹,Trussa Colin W.¹,McCrink Matthew¹

Affiliation:

1. Ohio State University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2488

Reference19 articles.

1. Internal Flow

2. CFD Models of a Serpentine Inlet, Fan, and Nozzle

3. Giuliani, J.E. "Jet Engine Fan Response to Inlet Distortions Generated by Ingested Boundary Layer Flow," Ph.D. Dissertation, Aeronautical and Astronautical Engineering Dept.The Ohio State University, Columbus, OH,2016.

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