Design and Experimental Study of a Turbojet VTOL Aircraft with One-Dimensional Thrust Vectoring Nozzles

Design and Experimental Study of a Turbojet VTOL Aircraft with One-Dimensional Thrust Vectoring Nozzles

Turbojet engines have a slow response and require mechanical assistance to perform vertical take-offs and landings. In this paper, we propose a vertical take-off and landing (VTOL) aircraft that contains one-dimensional thrust vectoring nozzle modules to solve the problem of dependence on the respon...

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Bibliographic Details
Main Authors: Benshan Liu, Yongsheng Gao, Liang Gao, Junming Zhang, Yanhe Zhu, Xizhe Zang, Jie Zhao
Format: Article
Language:English
Published: MDPI AG 2022-11-01
Series:Aerospace
Subjects:
thrust vectoring nozzle
turbojet aircraft
VTOL
Online Access:https://www.mdpi.com/2226-4310/9/11/678

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