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

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...

Volledige beschrijving

Bibliografische gegevens
Hoofdauteurs: K. Wu, Z. Liu, R. Deng, G. Zhang, Z. Zhu, V. R. P. Sethuraman, X. Su
Formaat: Artikel
Taal:English
Gepubliceerd in: Isfahan University of Technology 2023-01-01
Reeks:Journal of Applied Fluid Mechanics
Onderwerpen:
aerodynamics
aeronautics
supersonic nozzle
shock-induced thrust vector control
flow control
Online toegang:https://www.jafmonline.net/article_2179_bc962ffda3c200cd6cf6197e1565c97b.pdf

Internet

https://www.jafmonline.net/article_2179_bc962ffda3c200cd6cf6197e1565c97b.pdf

Gelijkaardige items