Flamelet Generated Manifolds for Partially Premixed, Highly Stretched and Non-Adiabatic Combustion in Gas Turbines-Reference-Cited by-同舟云学术

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Flamelet Generated Manifolds for Partially Premixed, Highly Stretched and Non-Adiabatic Combustion in Gas Turbines

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
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Author:

Klarmann Noah¹,Sattelmayer Thomas¹,Geng Weiqun²,Magni Fulvio²

Affiliation:

1. Technical University of Munich

2. GE Power

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. Modelling of Premixed Laminar Flames using Flamelet-Generated Manifolds

2. 2van Oijen, J. A., Flamelet-Generated Manifolds : Development and Application to Premixed Laminar Flames, Ph.D. thesis,Technische Universiteit Eindhoven, 2002.

3. A Premixed Flamelet−PDF Model for Biomass Combustion in a Grate Furnace

4. A five dimensional implementation of the flamelet generated manifolds technique for gas turbine application

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Measurements and simulations on effects of elevated pressure and strain rate on NOx emissions in laminar premixed NH3/CH4/air and NH3/H2/air flames;Fuel;2024-02

2. Canonical Validation of a Modeling Strategy for Carbon Monoxide Emissions in Staged Operation of Gas Turbine Combustors;Journal of the Global Power and Propulsion Society;2020-11-13

3. Linearized Euler Equations for the Prediction of Linear High-Frequency Stability in Gas Turbine Combustors;Journal of Engineering for Gas Turbines and Power;2016-10-04

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