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Relevant bibliographies by topics / Aircraft gas-turbines Combustion chambers

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Dissertations / Theses

Academic literature on the topic 'Aircraft gas-turbines Combustion chambers'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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Dissertations / Theses on the topic "Aircraft gas-turbines Combustion chambers"

1

Birmaher, Shai. "A method for aircraft afterburner combustion without flameholders." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28081.

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Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2009.<br>Committee Chair: Zinn, Ben; Committee Member: Fuller, Thomas; Committee Member: Gaeta, Rick; Committee Member: Jagoda, Jeff; Committee Member: Neumeier, Yedidia

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2

Acharya, Vishal Srinivas. "Dynamics of premixed flames in non-axisymmetric disturbance fields." Diss., Georgia Institute of Technology, 2013. http://hdl.handle.net/1853/50213.

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With strict environmental regulations, gas turbine emissions have been heavily constrained. This requires operating conditions wherein thermo-acoustic flame instabilities are prevalent. During this process the combustor acoustics and combustion heat release fluctuations are coupled and can cause severe structural damage to engine components, reduced operability, and inefficiency that eventually increase emissions. In order to develop an engine without these problems, there needs to be a better understanding of the physics behind the coupling mechanisms of this instability. Among the several co

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3

Bobba, Mohan Krishna. "Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/26502.

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Thesis (Ph.D)--Aerospace Engineering, Georgia Institute of Technology, 2008.<br>Committee Chair: Seitzman, Jerry; Committee Member: Filatyev, Sergei; Committee Member: Jagoda, Jechiel; Committee Member: Lieuwen, Timothy; Committee Member: Shelton, Samuel; Committee Member: Zinn, Ben. Part of the SMARTech Electronic Thesis and Dissertation Collection.

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4

Wang, Hongjuan. "Simulation of fuel injectors excited by synthetic microjets." Thesis, Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/11862.

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5

Crawford, Jackie H. III. "Factors that limit control effectiveness in self-excited noise driven combustors." Diss., Georgia Institute of Technology, 2012. http://hdl.handle.net/1853/43647.

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A full Strouhal number thermo-acoustic model is purposed for the feedback control of self excited noise driven combustors. The inclusion of time delays in the volumetric heat release perturbation models create unique behavioral characteristics which are not properly reproduced within current low Strouhal number thermo acoustic models. New analysis tools using probability density functions are introduced which enable exact expressions for the statistics of a time delayed system. Additionally, preexisting tools from applied mathematics and control theory for spectral analysis of time delay sy

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6

Ku, Shiuh-Huei. "An investigation of the gas fired pulsating combustor." Diss., Georgia Institute of Technology, 1988. http://hdl.handle.net/1853/13062.

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7

Neumeier, Yedidia. "Frequency domain analysis of a gas fired mechanically valved pulse combustor." Diss., Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/13354.

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8

Lieuwen, Tim C. "Investigation of combustion instability mechanisms in premixed gas turbines." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/20300.

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9

Bainbridge, William David Quillen. "The numerical similation of oscillations in gas turbine combustion chambers." Thesis, University of Cambridge, 2014. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.648428.

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10

Cavaliere, Davide Egidio. "Blow-off in gas turbine combustors." Thesis, University of Cambridge, 2014. https://www.repository.cam.ac.uk/handle/1810/265575.

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This thesis describes an experimental investigation of the flame structure close to the extinction and the blow-off events of non-premixed and spray flames stabilized on an axisymmetric bluff body in a confined swirl configuration. The comparison of flames of different canonical types in the same basic aerodynamic field allows insights on the relative blow-off behaviour. The first part of the thesis describes several velocity measurements in non-reacting and reacting flows. The main usefulness of this data is to provide the aerodynamic flow pattern and some discussion on the velocity field and

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