Project 28, Area 4: Combustion Model Development and Evaluation

Menon, Suresh; Sun, Wenting; Lu, Tianfeng; Panchal, A.; Yang, Suo; Gao, Xiang; Gao, Yang; Park, Ji-Woong

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Project 28, Area 4: Combustion Model Development and Evaluation

2017-12-01
By Menon, Suresh ; Sun, Wenting ; Lu, Tianfeng

File Language:

English

Details

Alternative Title:

Combustion Model Development and Evaluation
Creators:

Menon, Suresh ; Sun, Wenting ; Lu, Tianfeng ; Panchal, A. ; Yang, Suo ; Gao, Xiang ; Gao, Yang ; Park, Ji-Woong
Corporate Creators:

Georgia Institute of Technology. School of Aerospace Engineering
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Center of Excellence for Alternative Jet Fuels and Environment ; United States. Department of Transportation. Federal Aviation Administration. Office of Environment and Energy
Subject/TRT Terms:
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. Center of Excellence for Alternative Jet Fuels and Environment
Abstract:

This project is developing computational tools needed to evaluate alternate fuel combustion in a spray combustion system. The configuration chosen for final study is a subscale Referee combustor designed to investigate lean blow out (LBO) as a function of alternate fuel properties. The computational task requires development of reduced reaction kinetics for these fuels, spray fuel properties and integration into a large-eddy simulation (LES) solver. This project developed a reduced reaction kinetic model and investigated techniques for kinetics acceleration and then applied these models into an LES solver model. The Referee rig is simulated for 3 different fuels for both near blow out (NBO) and LBO. Analysis of the simulations identified critical needs for proper boundary conditions characterization and inclusion of multi-component fuel properties. Although later studies were funded by NASA (in Years 2-3), the initial study under this project demonstrated the viability of LES to study such fuel dependent kinetics in a complex gas turbine combustor.
Format:

PDF
Funding:

13-C-AJFE-GIT-028
Download URL:

https://rosap.ntl.bts.gov/view/dot/89771/dot_89771_DS1.pdf
File Type:

[PDF - 2.74 MB]
Collection(s):

Federal Aviation Administration
Main Document Checksum:

urn:sha-512:09b2e9cf6c80b95f6163f0b823689374c6e705507fcc57cb3f7c9bed264d547bdac6566775472eabc16219a8cbc7d4b7ae78c98320fe63b88b4e99991fd64cb8

File Language:

English

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