Low Frequencies and Growth of Oscillations in a Rijke Tube

R.P. Mushini,; K. Ramamurthi,

doi:10.1515/TJJ.2007.24.3-4.223

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Low Frequencies and Growth of Oscillations in a Rijke Tube

R.P. Mushini, und K. Ramamurthi,

Veröffentlicht/Copyright: 1. Dezember 2007

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 24 Heft 3-4

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APA
Harvard
Chicago
Vancouver

Mushini,, R.P. and Ramamurthi,, K.. "Low Frequencies and Growth of Oscillations in a Rijke Tube" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 223-230. https://doi.org/10.1515/TJJ.2007.24.3-4.223

Mushini,, R. & Ramamurthi,, K. (). Low Frequencies and Growth of Oscillations in a Rijke Tube. International Journal of Turbo and Jet Engines, 24(3-4), 223-230. https://doi.org/10.1515/TJJ.2007.24.3-4.223

Mushini,, R. and Ramamurthi,, K. () Low Frequencies and Growth of Oscillations in a Rijke Tube. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 223-230. https://doi.org/10.1515/TJJ.2007.24.3-4.223

Mushini,, R.P. and Ramamurthi,, K.. "Low Frequencies and Growth of Oscillations in a Rijke Tube" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 223-230. https://doi.org/10.1515/TJJ.2007.24.3-4.223

Mushini, R, Ramamurthi, K. Low Frequencies and Growth of Oscillations in a Rijke Tube. International Journal of Turbo and Jet Engines. ;24(3-4): 223-230. https://doi.org/10.1515/TJJ.2007.24.3-4.223

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Published Online: 2007-12

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Artikel in diesem Heft

CONTENTS
Microturbine Performance Testing with Twin Rotating Disk Regenerators
Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model
Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method
A Phenomenological Two-Phase Flow Model of Atomization in an Internally Mixed Liquid Atomizer
Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor
An Experimental Investigation on the Airflow in Twin Submerged Side Intake at Subsonic Speeds
Low Frequencies and Growth of Oscillations in a Rijke Tube
Gas Turbine Diagnostics Under Variable Operating Conditions
Effect of the Second Stage on a Partially Admitted Small Turbine
Probabilistic Analysis of a Turbine Blade

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https://doi.org/10.1515/TJJ.2007.24.3-4.223

Artikel in diesem Heft

CONTENTS
Microturbine Performance Testing with Twin Rotating Disk Regenerators
Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model
Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method
A Phenomenological Two-Phase Flow Model of Atomization in an Internally Mixed Liquid Atomizer
Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor
An Experimental Investigation on the Airflow in Twin Submerged Side Intake at Subsonic Speeds
Low Frequencies and Growth of Oscillations in a Rijke Tube
Gas Turbine Diagnostics Under Variable Operating Conditions
Effect of the Second Stage on a Partially Admitted Small Turbine
Probabilistic Analysis of a Turbine Blade