Study on the Aerodynamic Performance of Novel Bypass Shock-Induced Thrust Vector Nozzle

This article studies the aerodynamic performance of a novel bypass shock-induced thrust vector nozzle. An arc-shaped bypass is innovatively designed to optimize nozzle performance and equips a variable shrinkage part. The nozzle performance is investigated numerically under diverse shrinkage area ra...

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Bibliographic Details
Main Authors: K. Wu, Z. Liu, R. Deng, G. Zhang, Z. Zhu, V. R. P. Sethuraman, X. Su
Format: Article
Language:English
Published: Isfahan University of Technology 2023-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:https://www.jafmonline.net/article_2179_bc962ffda3c200cd6cf6197e1565c97b.pdf