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Compressible Turbulent Flame Speed of Highly Turbulent Standing Flames
- Date Issued:
- 2018
- Abstract/Description:
- This work presents the first measurement of turbulent burning velocities of a highly-turbulent compressible standing flame induced by shock-driven turbulence in a Turbulent Shock Tube. High-speed schlieren, chemiluminescence, PIV, and dynamic pressure measurements are made to quantify flame-turbulence interaction for high levels of turbulence at elevated temperatures and pressure. Distributions of turbulent velocities, vorticity and turbulent strain are provided for regions ahead and behind the standing flame. The turbulent flame speed is directly measured for the high-Mach standing turbulent flame. From measurements of the flame turbulent speed and turbulent Mach number, transition into a non-linear compressibility regime at turbulent Mach numbers above 0.4 is confirmed, and a possible mechanism for flame generated turbulence and deflagration-to-detonation transition is established.
Title: | Compressible Turbulent Flame Speed of Highly Turbulent Standing Flames. |
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Name(s): |
Sosa, Jonathan, Author Ahmed, Kareem, Committee Chair Kassab, Alain, Committee Member Kapat, Jayanta, Committee Member University of Central Florida, Degree Grantor |
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Type of Resource: | text | |
Date Issued: | 2018 | |
Publisher: | University of Central Florida | |
Language(s): | English | |
Abstract/Description: | This work presents the first measurement of turbulent burning velocities of a highly-turbulent compressible standing flame induced by shock-driven turbulence in a Turbulent Shock Tube. High-speed schlieren, chemiluminescence, PIV, and dynamic pressure measurements are made to quantify flame-turbulence interaction for high levels of turbulence at elevated temperatures and pressure. Distributions of turbulent velocities, vorticity and turbulent strain are provided for regions ahead and behind the standing flame. The turbulent flame speed is directly measured for the high-Mach standing turbulent flame. From measurements of the flame turbulent speed and turbulent Mach number, transition into a non-linear compressibility regime at turbulent Mach numbers above 0.4 is confirmed, and a possible mechanism for flame generated turbulence and deflagration-to-detonation transition is established. | |
Identifier: | CFE0007102 (IID), ucf:51955 (fedora) | |
Note(s): |
2018-05-01 M.S.A.E. Engineering and Computer Science, Mechanical and Aerospace Engineering Masters This record was generated from author submitted information. |
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Subject(s): | compressible turbulent flames -- turbulence -- combustion -- standing flames | |
Persistent Link to This Record: | http://purl.flvc.org/ucf/fd/CFE0007102 | |
Restrictions on Access: | campus 2023-05-15 | |
Host Institution: | UCF |