Techniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review

S Afridi, TA Khan, SIA Shah, TA Shams, K Mohiuddin… - Energies, 2023 - mdpi.com
Thrust vectoring innovations are demonstrated ideas that improve the projection of
aerospace power with enhanced maneuverability, control effectiveness, survivability …

Numerical Investigation on the Thrust Vectoring Performance of Bypass Dual Throat Nozzle

S Afridi, TA Khan, SIA Shah, TA Shams, K Mehmood… - Energies, 2023 - mdpi.com
Modern aircraft and missiles are gradually integrating thrust vector control systems to
enhance their military capabilities. Bypass Dual-Throat Nozzle (BDTN) control is a new …

A shape design optimization methodology based on the method of characteristics for rocket nozzles

T Fernandes, A Souza, F Afonso - CEAS Space Journal, 2023 - Springer
Even though shape optimization is a powerful tool for designing aerospace vehicles, it can
be time-consuming when high-fidelity models are employed. Thus, lower-fidelity simulations …

On the thrust vector performance optimization and modeling of supersonic split line nozzles

D Li, G Wang, J Cheng, H Yang - International Journal of Heat and Mass …, 2025 - Elsevier
The supersonic split line (SSSL) nozzle is one of the thrust vector nozzles. Because of the
complex internal flow, designing a high-performance SSSL nozzle, especially with a large …

Effect of Bypass Duct on the Thrust Vectoring Performance of Dual Throat Nozzle in a Supersonic Aircraft

S Afridi, TA Khan, I Shah, Y Ali… - Journal of Fluids …, 2024 - asmedigitalcollection.asme.org
Due to its ability to maximize thrust vectoring performance, the bypass dual throat nozzle
(BDTN) has an advantage over other fluidic vectoring controls. In this study, numerical …

Optimization of bypass flow introduction angle in dual-throat nozzle

S Bharali, S Joshi, M Zunaid - Journal of Electrical Systems, 2024 - search.proquest.com
This research paper investigates the optimal angle for introducing a bypass jet in rocket
engines for thrust vectoring. Numerical simulations using a finite-volume method were …

A study on the performance of a swirling–straight composite nozzle

D Yu, S Li, J Zhang, N Wang… - Asia‐Pacific Journal of …, 2024 - Wiley Online Library
The nozzle is the key component of water mist fire extinguishing system. As a response to
the problems of small injection angle associated with straight jet nozzles and the weak axial …

A Detailed Experimental Investigation Into the Vectoring Performance of Asymmetric Bypass Dual Throat Nozzles

S Weigert, B Crowther, MK Quinn… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
Bypass dual throat nozzles (BDTN) was first proposed in the 1990s as means to enable
more effective and efficient control of combat aircraft, but real-world implementation has not …

[PDF][PDF] Techniques of Fluidic Thrust Vectoring in Jet Engine Nozzles: A Review. Energies 2023, 16, 5721

S Afridi, TA Khan, SIA Shah, TA Shams, K Mohiuddin… - 2023 - pdfs.semanticscholar.org
Thrust vectoring innovations are demonstrated ideas that improve the projection of
aerospace power with enhanced maneuverability, control effectiveness, survivability …

Design and Optimization of Rocket Engine Nozzle Flow Field Based on Multi-Objective Optimization Algorithm

C Yunfeng - 2024 3rd International Conference on Data …, 2024 - ieeexplore.ieee.org
Morphology optimization is an effective approach for designing rocket engine nozzles, but it
can be time-consuming when using high-fidelity models. Therefore, in the early design …