Search
Now showing items 1-3 of 3
Experimental Measurement Of Flame Response To Acoustic Oscillations
(2014-06-20)
Acoustic instabilities in a combustion chamber arise due to the coupling of acoustic pressure with in-phase heat-release, and are characterized by large amplitude oscillations of one or more natural modes of combustor. ...
Combustion Instability Screech In Gas Turbine Afterburner
(2009-08-04)
Gas turbine reheat thrust augmenters known as afterburners are used to provide additional thrust during emergencies, take off, combat, and in supersonic flight of high-performance aircrafts. During the course of reheat ...
Studies On Impinging-Jet Atomizers
(2009-05-06)
Characteristics of impinging-jet atomizers in the context of application in liquid propulsion systems are studied in this thesis. A review of past studies on impinging jets revealed the necessity of a correlation in terms ...