Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation

Erich A. Wilson,; Dan Adler,; Pinhas Bar-Yoseph,

doi:10.1515/TJJ.2001.18.3.187

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Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation

Erich A. Wilson, , Dan Adler, and Pinhas Bar-Yoseph,

Published/Copyright: September 1, 2001

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From the journal International Journal of Turbo and Jet Engines Volume 18 Issue 3

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APA
Harvard
Chicago
Vancouver

Wilson,, Erich A., Adler,, Dan and Bar-Yoseph,, Pinhas. "Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation" International Journal of Turbo and Jet Engines, vol. 18, no. 3, 2001, pp. 187-200. https://doi.org/10.1515/TJJ.2001.18.3.187

Wilson,, E., Adler,, D. & Bar-Yoseph,, P. (2001). Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation. International Journal of Turbo and Jet Engines, 18(3), 187-200. https://doi.org/10.1515/TJJ.2001.18.3.187

Wilson,, E., Adler,, D. and Bar-Yoseph,, P. (2001) Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation. International Journal of Turbo and Jet Engines, Vol. 18 (Issue 3), pp. 187-200. https://doi.org/10.1515/TJJ.2001.18.3.187

Wilson,, Erich A., Adler,, Dan and Bar-Yoseph,, Pinhas. "Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation" International Journal of Turbo and Jet Engines 18, no. 3 (2001): 187-200. https://doi.org/10.1515/TJJ.2001.18.3.187

Wilson, E, Adler, D, Bar-Yoseph, P. Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation. International Journal of Turbo and Jet Engines. 2001;18(3): 187-200. https://doi.org/10.1515/TJJ.2001.18.3.187

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Unsteady Analysis of a Time-Dependent Hot Streak in a Turbine Stage
A Study on Straight Flow Annular Combustor for Small Scale Turbojet Engine
Radial Cascade Unsteady Airfoil Theory
Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation
Multi-Objective Optimization of Turbomachinery Cascades for Minimum Loss, Maximum Loading, and Maximum Gap-to-Chord Ratio
Some Unconventional Applications of Thermometers in Turbomachinery
A Repeating Stage Model in Flow Predictions of Axial Flow Compressor Rear Stages

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https://doi.org/10.1515/TJJ.2001.18.3.187

Articles in the same Issue

CONTENTS
Unsteady Analysis of a Time-Dependent Hot Streak in a Turbine Stage
A Study on Straight Flow Annular Combustor for Small Scale Turbojet Engine
Radial Cascade Unsteady Airfoil Theory
Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation
Multi-Objective Optimization of Turbomachinery Cascades for Minimum Loss, Maximum Loading, and Maximum Gap-to-Chord Ratio
Some Unconventional Applications of Thermometers in Turbomachinery
A Repeating Stage Model in Flow Predictions of Axial Flow Compressor Rear Stages