Multi-objective optimization design of S-shaped inlet with internal bump-Reference-Cited by-同舟云学术

Multi-objective optimization design of S-shaped inlet with internal bump

Published:2022-11 Issue: Volume:130 Page:107901
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

He Yu-Bo,Yang Qing-Zhen,Shi Yong-Qiang,Gao Xiang^ORCID,Yang Hui-Cheng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

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2. Influence of cross-sectional shape on the flow in a highly bent research intake duct for jet engines;Haug,2017

3. Flow characteristics of an ultracompact serpentine inlet with an internal bump;Sun;J. Aerosp. Eng.,2018

4. Flow structure and performance characteristics of X-47-like slot-shaped inlet;Zhang;Acta Aeronaut. Astronaut. Sin.,2009

5. Numerical simulation of power and flow field characteristics of conformal intake and exhaust for flying wing unmanned aerial vehicle;Zhang;J. Northwest. Polytech. Univ.,2015

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