ERD

Centrifugal Compressor Surge in Closed-Loop Systems: Initial Modeling and Comparison With Experiments

Project: INSPIRE

Updated at: 01-11-2024

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Project acronym INSPIRE

Development of 1D Model of Constant-Volume Combustor and Numerical Analysis of the Exhaust Nozzle

Project: INSPIRE

Updated at: 01-11-2024

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Project acronym INSPIRE

Thickened Flame LES methodology for turbulent propagating flames in non-homogeneous mixtures: application to a constant ...

Project: INSPIRE

Updated at: 01-11-2024

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Project acronym INSPIRE

Numerical Analysis and Design of New Exhaust Section Downstream of Constant Volume Combustor

Project: INSPIRE

Updated at: 01-11-2024

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Project acronym INSPIRE

Swirling Flow Effects on Highly-Heated Aerospike Nozzle Jets

Project: INSPIRE

Updated at: 01-11-2024

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Project acronym INSPIRE

Test of Transeo Code, equipped with literature performance maps

Project: INSPIRE

Updated at: 21-06-2024

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Project acronym INSPIRE

Public Dissemination: Mid-programme workshop, ICVDCW 2021

Project: INSPIRE

Updated at: 21-06-2024

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Project acronym INSPIRE

Exploring the deflagration-autoignition-detonation transition in the context of pressure gain combustion

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Effects of Increased RDC Injector Diodicity

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Numerical investigation of the combustion modes resulting from the auto-ignition of hot spots in hydrogen air mixtures

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

A Review of Recent Advances in the Combustor and Blade Cooling Methods for Pressure Gain Applications

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Techno-economic analysis of innovative solutions for island grids with high renewable solar share

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

A Methodology for Optimizing Turbines powered by Rotating Detonation Combustors

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

An investigation of modelling parameters for surge phenomenon in axial compressors

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Extension of a Low-order Model for Detonation Velocity Suppression in Rotation Detonation Combustors

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Computational Aeroacoustics for a Cold, Non-Ideally Expanded Aerospike Nozzle

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Periodic Reporting for period 1 - INSPIRE (INSpiring Pressure gain combustion Integration, Research, and Education)

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Experimental characterization of ignition events in CVC like conditions

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Experimental Comparison of Different Pressure Gain Measurement Techniques for RDCs

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Experimental characterization of ignition events in CVC like conditions

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Large Eddy Simulation of a Pistonless Constant Volume Combustor: A New Concept of Pressure Gain Combustion

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Establish website & secure portal

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Development and Validation of a 0-D/1-D Model to Evaluate Pulsating Conditions from a Constant Volume Combustor

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Exploring the deflagration-autoignition-detonation transition in the context of pressure gain combustion (work in progre...

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Analysis of a Co-Flow Mixer in Preparation of Combustor-Turbine Matching in a Rotating Detonation Engine

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

EXPLORING THE DEFLAGRATION-AUTOIGNITION-DETONATION TRANSITION IN THE CONTEXT OF PESSUE GAIN COMBUSTION

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Phase Averaged Static Pressure Fields Inside a Rotating Detonation Combustor

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Experimental characterization of ignition events in CVC like conditions

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Quantification of Heat Loads for Rotating Detonation Combustor with Gas Turbine Conditions

Project: INSPIRE

Updated at: 28-04-2024

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Project acronym INSPIRE

Resources

Selected filters:

Centrifugal Compressor Surge in Closed-Loop Systems: Initial Modeling and Comparison With Experiments

Development of 1D Model of Constant-Volume Combustor and Numerical Analysis of the Exhaust Nozzle

Thickened Flame LES methodology for turbulent propagating flames in non-homogeneous mixtures: application to a constant ...

Numerical Analysis and Design of New Exhaust Section Downstream of Constant Volume Combustor

Swirling Flow Effects on Highly-Heated Aerospike Nozzle Jets

Test of Transeo Code, equipped with literature performance maps

Public Dissemination: Mid-programme workshop, ICVDCW 2021

Exploring the deflagration-autoignition-detonation transition in the context of pressure gain combustion

Effects of Increased RDC Injector Diodicity

Numerical investigation of the combustion modes resulting from the auto-ignition of hot spots in hydrogen air mixtures

A Review of Recent Advances in the Combustor and Blade Cooling Methods for Pressure Gain Applications

Techno-economic analysis of innovative solutions for island grids with high renewable solar share

A Methodology for Optimizing Turbines powered by Rotating Detonation Combustors

An investigation of modelling parameters for surge phenomenon in axial compressors

Extension of a Low-order Model for Detonation Velocity Suppression in Rotation Detonation Combustors

Computational Aeroacoustics for a Cold, Non-Ideally Expanded Aerospike Nozzle

Low-Order Model for Detonation Velocity Suppression in Rotating Detonation Combustors

Periodic Reporting for period 1 - INSPIRE (INSpiring Pressure gain combustion Integration, Research, and Education)

Experimental characterization of ignition events in CVC like conditions

Experimental Comparison of Different Pressure Gain Measurement Techniques for RDCs

Experimental characterization of ignition events in CVC like conditions

Large Eddy Simulation of a Pistonless Constant Volume Combustor: A New Concept of Pressure Gain Combustion

Establish website & secure portal

Development and Validation of a 0-D/1-D Model to Evaluate Pulsating Conditions from a Constant Volume Combustor

Exploring the deflagration-autoignition-detonation transition in the context of pressure gain combustion (work in progre...

Analysis of a Co-Flow Mixer in Preparation of Combustor-Turbine Matching in a Rotating Detonation Engine

EXPLORING THE DEFLAGRATION-AUTOIGNITION-DETONATION TRANSITION IN THE CONTEXT OF PESSUE GAIN COMBUSTION

Phase Averaged Static Pressure Fields Inside a Rotating Detonation Combustor

Experimental characterization of ignition events in CVC like conditions

Quantification of Heat Loads for Rotating Detonation Combustor with Gas Turbine Conditions