Results 11 to 20 of about 16,840 (258)

Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode

open access: yesInternational Journal of Aerospace Engineering
The ejector mode of the Rocket-Based Combined-Cycle (RBCC) engine is characterized by high fuel consumption. This study is aimed at investigating the influence of the rocket fuel-rich degree on the RBCC engine’s performance under the ejector mode ...
Yizhi Yao   +9 more
doaj   +2 more sources

Supersonic Combustion Mode Analysis of a Cavity Based Scramjet

open access: yesAerospace, 2022
Since flame stability is the key to the performance of scramjets, scramjet combustion mode and instability characteristics were investigated by using the POD method based on a cavity-stabilized scramjet. Experiments were developed on a directly connected
Yu Meng   +4 more
doaj   +2 more sources

Comparison of Dual-Combustion Ramjet and Scramjet Performances Considering Combustion Efficiency

open access: yesApplied Sciences, 2022
The performances of a dual-combustion ramjet (DCR) and a scramjet were compared via computational fluid dynamics numerical simulation to provide theoretical guidance for engine selection for a hypersonic vehicle.
Xianju Wu, Zhijun Wei
doaj   +2 more sources

The Combustion Characteristics of Double Ramps in a Strut-Based Scramjet Combustor

open access: yesEnergies, 2021
This paper focuses on the influence of ramp locations upstream of a strut-based scramjet combustor under reacting flow conditions that are numerically investigated. In contrast, a computational study is adopted using Reynolds Averaged Navier Stokes (RANS)
A. Antony Athithan   +4 more
doaj   +2 more sources

A Study on a Vitiated Air Heater for a Direct-Connect Scramjet Combustor and Preliminary Test on the Scramjet Combustor Ignition

open access: yesAerospace, 2023
Vitiation air heater (VAH) combustion characteristics for a direct-connect scramjet combustor (DCSC) were experimentally studied. The VAH consists of a head, modular chamber, and circular-to-rectangular shape transition (CRST) nozzle.
Jae-Hyuk Lee   +4 more
semanticscholar   +1 more source

Research progress on solid-fueled Scramjet

open access: yesChinese Journal of Aeronautics, 2021
The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet. It shows significant advantages such as simple fuel supply and compactness, avoiding the complex system of tanks and pipelines that encountered in liquid-fueled ...
Xiang Zhao   +6 more
semanticscholar   +1 more source

Recent Advancements in Design Optimization of Lattice‐Structured Materials

open access: yesAdvanced Engineering Materials, Volume 25, Issue 17, September 2023., 2023
Enhancement in the performance of lattice materials involves improving the design in the manufacturing process. Functional gradation and multimorphology strategies are utilized to enhance the multifunctionality of lattice materials. As the preceding strategies involve challenges and limitations, utilizing them concurrently with automated design ...
Abdulla Alhembar   +4 more
wiley   +1 more source

Prediction of Equivalence Ratio in Combustion Flame Using Chemiluminescence Emission and Deep Neural Network

open access: yesInternational Journal of Energy Research, Volume 2023, Issue 1, 2023., 2023
A reliable combustion monitoring system is essential to satisfy global carbon neutrality trends. As the concentrations of emissions and flame stability are associated with the air–fuel ratio, the equivalence ratio should be continuously evaluated. In this study, a deep neural network‐ (DNN‐) based regression model is proposed to predict the equivalence
Sanghun Shin   +4 more
wiley   +1 more source

Review on Creep Phenomenon and Its Model in Aircraft Engines

open access: yesInternational Journal of Aerospace Engineering, Volume 2023, Issue 1, 2023., 2023
The aircraft is subjected to high‐temperature and high‐pressure conditions during flight, which renders it susceptible to the occurrence of creep phenomenon. Several academics have conducted extensive research on this issue. This research paper provides a comprehensive overview of the existing literature on creep phenomena in aircraft engines.
Lin Yuan   +7 more
wiley   +1 more source

Sizing of scramjet vehicles [PDF]

open access: yesProgress in Propulsion Physics, 2011
The current European project LAPCAT II has the ambitious goal to de¦ne a conceptual vehicle capable of achieving the antipodal range Brussels Sydney (∼ 18,000 km) in about 2 h at Mach number Ma = 8. At this high speed, the requirement of high lift to drag (L/D) ratio is critical to high performance, because of high skin friction and wave drag: in fact,
INGENITO, ANTONELLA, GULLI S, BRUNO C.
openaire   +2 more sources

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