Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine

Stanislaw Antas,; Tadeusz Chmielniak,

doi:10.1515/TJJ.2008.25.3.197

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Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine

Stanislaw Antas, and Tadeusz Chmielniak,

Published/Copyright: September 1, 2008

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From the journal International Journal of Turbo and Jet Engines Volume 25 Issue 3

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MLA
APA
Harvard
Chicago
Vancouver

Antas,, Stanislaw and Chmielniak,, Tadeusz. "Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine" International Journal of Turbo and Jet Engines, vol. 25, no. 3, 2008, pp. 197-208. https://doi.org/10.1515/TJJ.2008.25.3.197

Antas,, S. & Chmielniak,, T. (2008). Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine. International Journal of Turbo and Jet Engines, 25(3), 197-208. https://doi.org/10.1515/TJJ.2008.25.3.197

Antas,, S. and Chmielniak,, T. (2008) Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine. International Journal of Turbo and Jet Engines, Vol. 25 (Issue 3), pp. 197-208. https://doi.org/10.1515/TJJ.2008.25.3.197

Antas,, Stanislaw and Chmielniak,, Tadeusz. "Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine" International Journal of Turbo and Jet Engines 25, no. 3 (2008): 197-208. https://doi.org/10.1515/TJJ.2008.25.3.197

Antas, S, Chmielniak, T. Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine. International Journal of Turbo and Jet Engines. 2008;25(3): 197-208. https://doi.org/10.1515/TJJ.2008.25.3.197

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Articles in the same Issue

CONTENTS
Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
Active and Passive Flow Control in a Turbine Cascade
Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
Turbomachine Shrouded Rotor Blade Forced Response Analysis
Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
Performance Improvement of Gas Turbine Cycles
Characteristics of Supersonic Impinging Moist Air Jets

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https://doi.org/10.1515/TJJ.2008.25.3.197

Articles in the same Issue

CONTENTS
Reduced-Order Model of a Mistuned Multi-Stage Bladed Rotor
Active and Passive Flow Control in a Turbine Cascade
Effects of Geometric and Structural Parameters on Coupled Bending Torsion Flutter in Turbo Machinery Blades
Turbomachine Shrouded Rotor Blade Forced Response Analysis
Numerical Investigation on Multi-cycle Operation of Pulse Detonation Rocket Engine
Determination of Performance and Parameters for Turboprop and Turboshaft Engine for Modification through Change of Gas Temperature Before Turbine
Performance Improvement of Gas Turbine Cycles
Characteristics of Supersonic Impinging Moist Air Jets