Results 131 to 140 of about 2,502 (163)
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Dynamic Experimental Investigations of a Bypass Dual Throat Nozzle
Journal of Engineering for Gas Turbines and Power, 2015The 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
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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
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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
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Analysis of mixing enhancement ability of bypass dual throat nozzle with single/multi-tabs
Heat Transfer EngineeringBypass 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
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Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020The 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
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
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, 2022Thrust vectoring is a promising technology that offers the potential for improved maneuverability, control efficiency, and stealth characteristics of aircraft.
Saadia Afridi, Tariq Amin Khan
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An application of machine learning for geometric optimization of a dual-throat bent nozzle
Advances in Engineering SoftwareHomin Kim +3 more
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Calculation method for fluidic thrust-vectoring dual throat nozzle
Other Conferences, 2022A 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
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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

