Results 141 to 150 of about 2,502 (163)
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Experimental Investigation into the Vectoring Performance of Asymmetric Bypass Dual Throat Nozzles

AIAA Journal
Bypass dual throat nozzles were first proposed in the 1990s as a means to enable more effective and efficient control of combat aircraft, but real-world implementation has not yet been demonstrated. In an attempt to mitigate this gap, this study provides
Samuel Weigert   +3 more
semanticscholar   +1 more source

Performance Analyses of Fluidic Thrust Vector Control System Using Dual Throat Nozzle

AIAA Propulsion and Energy 2019 Forum, 2019
Flows in the rocket engine nozzles have been numerically analyzed to assess the performance of thrust vector control system of fluidic type by the direct simulation Monte Carlo method.
Y. Maruyama   +2 more
semanticscholar   +1 more source

Preliminary Design and Analysis of a Dual Throat Fluidic Thrust Vectoring Nozzle for Supersonic Aerospace Application

SAE technical paper series
The Dual Throat Nozzle (DTN) is a unique nozzle configuration that enables fluidic thrust vectoring (FTV), improving aircraft maneuverability while reducing the mechanical complexity of traditional vectoring systems.
Vignesh Suresh   +5 more
semanticscholar   +1 more source

Numerical Investigation on Aerodynamic Vector Performance of a Axisymmetric Bypass Dual Throat Nozzle

2023
Xuefeng Xia   +6 more
openaire   +1 more source

Numerical study of secondary mass flow modulation in a Bypass Dual-Throat Nozzle

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021
Mohammad Hadi Hamedi Estakhrsar   +1 more
exaly  

Experimental evaluation and numerical simulation of performance of the bypass dual throat nozzle

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021
Mohammad Hadi Hamedi Estakhrsar   +1 more
exaly  

Outlet Temperature Field of Bypass Dual Throat Nozzles

Haijie Liang   +4 more
openaire   +1 more source

Experimental and Numerical Investigations of Bypass Dual-Throat Nozzle with Asymmetric Rear Configuration

2025 International Conference of Mechanical Engineering on Aerospace (CoMEA)
Shuai HUANG   +5 more
openaire   +1 more source

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