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Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle

Journal of Engineering for Gas Turbines and Power, 2015
The bypass dual throat nozzle (BDTN) does not consume any secondary injection from the other part of the engine, while it can produce steady and efficient vectoring deflection similar to the conventional dual throat nozzle (DTN). A BDTN model has been designed and subjected to dynamic experimental study.
Rui Gu, Jinglei Xu
openaire   +2 more sources

Optimization of bypass dual throat nozzle for thrust vectoring using improved HHO and RBF surrogate model

Materials Research Proceedings
Abstract. The optimization of aerospace propulsion systems plays a pivotal role in enhancing performance and efficiency. This paper presents a comprehensive analysis of a 2D bypass dual throat nozzle, with a primary focus on optimizing two critical design parameters: expansion ratio and bypass width, to maximize the mass flow rate and facilitate thrust
Arun Ravindranath
openaire   +2 more sources

Analysis of mixing enhancement ability of bypass dual throat nozzle with single/multi-tabs

Heat Transfer Engineering
Bypass dual throat nozzle (BDTN) represents an innovative fluidic thrust vectoring nozzle capable of adjusting thrust vectoring angles through self-adaptive flow control.
Ruifeng Pan   +4 more
openaire   +2 more sources

Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020
The dual throat nozzle achieves higher thrust vectoring efficiencies and lesser thrust loss than other fluidic thrust-vectoring nozzles. Separation always occurs at the bottom of the cavity with complex three-dimensional characteristics for the dual ...
Yangsheng Wang   +4 more
semanticscholar   +3 more sources

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

AIAA SCITECH 2025 Forum
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 yet been demonstrated. In an attempt to mitigate this gap, this study provides an extensive experimental investigation through conducting simultaneous pressure measurements ...
Samuel Weigert   +3 more
semanticscholar   +4 more sources

Multi-objective nozzle design optimization for maximum thrust vectoring performance

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022
Thrust vectoring is a promising technology that offers the potential for improved maneuverability, control efficiency, and stealth characteristics of aircraft.
Saadia Afridi, Tariq Amin Khan
semanticscholar   +1 more source

An application of machine learning for geometric optimization of a dual-throat bent nozzle

Advances in Engineering Software
Homin Kim   +3 more
semanticscholar   +3 more sources

Calculation method for fluidic thrust-vectoring dual throat nozzle

Other Conferences, 2022
A dual throat nozzle (DTN) is a novel type of fluidic thrust-vectoring (FTV) nozzle. Many computational studies have been done for DTNs. However, in general most efforts have only attained limited success.
Ye Chen   +5 more
semanticscholar   +1 more source

Research on the Afterbody Integration of BDTN and Exploration of Drag Reduction Methods

2025 International Conference of Mechanical Engineering on Aerospace (CoMEA)
The development trend of future combat aircraft capabilities represented by airplanes is wide speed range, high stealth ability, high maneuverability, and high energy.
Ruifeng Pan   +4 more
semanticscholar   +1 more source

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