30th Joint Propulsion Conference and Exhibit 1994
DOI: 10.2514/6.1994-3271
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Relation of CARS temperature fields to lean blowout performance in an aircraft gas turbine generic combustor

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Cited by 7 publications
(3 citation statements)
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“…This combustor is simpli ed from an experimental model. 25 The overall geometrical dimensions are kept the same as the experimental model, but the airjets on the upper and bottom walls are ignored.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…This combustor is simpli ed from an experimental model. 25 The overall geometrical dimensions are kept the same as the experimental model, but the airjets on the upper and bottom walls are ignored.…”
Section: Numerical Resultsmentioning
confidence: 99%
“…In this case, a simplified combustor from Switzer et al (1994) is used. The combustor length is about 0.6 meters.…”
Section: Formation In a Gas Turbine Combustormentioning
confidence: 99%
“…Several studies of different types of flames have proven its high capability [15][16][17][18]. Today, the CARS technique using the N 2 molecule as a temperature indicator is routinely used even in harsh combustion environments such as IC engines, high-pressure burners and gas turbines [19][20][21][22][23][24]. In order to probe temperatures in a technical relevant combustion chamber, optical access is always restricted by the need for very small windows.…”
Section: Introductionmentioning
confidence: 99%