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Journal Articles

One‐Dimensional High‐Speed Flows: Flow Patterns Derived for the Flow of Gases Through Nozzles, IncludingCompressibility and Viscosity Effects

J. Kestin, S.K. Zaremba

Aircraft Engineering (1953) 25 (6): 172–179.

https://doi.org/10.1108/eb032301

Published: 01 June 1953

View article titled, One‐Dimensional High‐Speed Flows: Flow Patterns Derived for the Flow of Gases Through Nozzles, IncludingCompressibility and Viscosity Effects

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Journal Articles

The Rapid Discharge of Gases from Vessels: An Explanation of Discrepancies Between Calculation and Experiment Explained by the Application of Wave Theory

J. Kestin, J.S. Glass

Aircraft Engineering (1951) 23 (10): 300–304.

https://doi.org/10.1108/eb032089

Published: 01 October 1951

View article titled, The Rapid Discharge of Gases from Vessels: An Explanation of Discrepancies Between Calculation and Experiment Explained by the Application of Wave Theory

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Journal Articles

The Reheat Factor in Turbines and Turbocompressors: New Formulae for Calculating the Factors for Units with Finite Stages Based on Known Methods Used on the Infinite Stage Assumption

J. Kestin, Ph.D., D.I.C., A.M.I.Mech.E.

Aircraft Engineering (1950) 22 (12): 361–367.

https://doi.org/10.1108/eb031976

Published: 01 December 1950

View article titled, The Reheat Factor in Turbines and Turbocompressors: New Formulae for Calculating the Factors for Units with Finite Stages Based on Known Methods Used on the Infinite Stage Assumption

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Journal Articles

Piston Velocities and Piston Work: The Influence of High Piston Velocities on the Pressure Distribution and Piston Work in Engine Cylinders

J.S. Glass, J. Kestin

Aircraft Engineering (1950) 22 (6): 163–165.

https://doi.org/10.1108/eb031907

Published: 01 June 1950

View article titled, Piston Velocities and Piston Work: The Influence of High Piston Velocities on the Pressure Distribution and Piston Work in Engine Cylinders

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Journal Articles

Thermodynamic Properties of Combustion Gases: A Simplified Basis for the Calculation of Gas Turbine Efficiencies in which all the Variables are Related to the Properties of Air by means of Determined Constants

J. Kestin, Ph.D., D.I.C., Dipl. Ing., A.M.I.Mech.E.

Aircraft Engineering (1948) 20 (8): 234–242.

https://doi.org/10.1108/eb031660

Published: 01 August 1948

View article titled, Thermodynamic Properties of Combustion Gases: A Simplified Basis for the Calculation of Gas Turbine Efficiencies in which all the Variables are Related to the Properties of Air by means of Determined Constants

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One‐Dimensional High‐Speed Flows: Flow Patterns Derived for the Flow of Gases Through Nozzles, IncludingCompressibility and Viscosity Effects

The Rapid Discharge of Gases from Vessels: An Explanation of Discrepancies Between Calculation and Experiment Explained by the Application of Wave Theory

The Reheat Factor in Turbines and Turbocompressors: New Formulae for Calculating the Factors for Units with Finite Stages Based on Known Methods Used on the Infinite Stage Assumption

Piston Velocities and Piston Work: The Influence of High Piston Velocities on the Pressure Distribution and Piston Work in Engine Cylinders

Thermodynamic Properties of Combustion Gases: A Simplified Basis for the Calculation of Gas Turbine Efficiencies in which all the Variables are Related to the Properties of Air by means of Determined Constants

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