Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method
The application of the Shock Vector Control (SVC) approach to an axysimmetric supersonic nozzle is studied numerically. SVC is a Fluidic Thrust Vectoring (FTV) strategy that is applied to fixed nozzles in order to realize jet-vectoring effects normally obtained by deflecting movable nozzles. In the...
Main Authors: | Emanuele Resta, Roberto Marsilio, Michele Ferlauto |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-12-01
|
Series: | Fluids |
Subjects: | |
Online Access: | https://www.mdpi.com/2311-5521/6/12/441 |
Similar Items
-
Study on the Aerodynamic Performance of Novel Bypass Shock-Induced Thrust Vector Nozzle
by: K. Wu, et al.
Published: (2023-01-01) -
Influence of Bypass Location on Two-Dimensional Shock Vectoring Nozzle
by: Bo-wen SHU, et al.
Published: (2023-09-01) -
Aerodynamic Characteristics of the Novel Two-Dimensional Enhanced Shock Vector Nozzle
by: Bowen Shu, et al.
Published: (2024-05-01) -
Fluidic Thrust, Propulsion, Vector Control of Supersonic Jets by Flow Entrainment and the Coanda Effect
by: Toshihiko Shakouchi, et al.
Published: (2022-11-01) -
Surface Pressure Measurement of Truncated, Linear Aerospike Nozzles Utilising Secondary Injection for Aerodynamic Thrust Vectoring
by: Jan Sieder-Katzmann, et al.
Published: (2024-06-01)