Hovering efficiency optimization of ducted propeller with large blade tip clearance based on grooved duct configuration-Reference-Cited by-同舟云学术

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Hovering efficiency optimization of ducted propeller with large blade tip clearance based on grooved duct configuration

Published:2024-07 Issue: Volume:150 Page:109226
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hu Yu^ORCID,Zhang Xu chao,Wang Guo qiang,Zhang Xue Peng,Li Han Zhen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference40 articles.

1. Review on ducted fans for compound rotorcraft;Zhang;Aeronaut. J.,2020

2. Aerodynamic performance of mutual interaction tandem propellers with ducted UAV;Rostami;Aerosp. Sci. Technol.,2021

3. Numerical investigations of ducted fan hover performance for FIW applications;Sheng,2015

4. Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion;Leifsson;Aerosp. Sci. Technol.,2013

5. Multidisciplinary exploration of DRAGON: an ONERA hybrid electric distributed propulsion concept;Schmollgruber,2019

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