Issue
Licensed
Unlicensed
Requires Authentication
Volume 17, Issue 4
Contents
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Requires Authentication UnlicensedCONTENTSLicensedDecember 1, 2000
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Requires Authentication UnlicensedExperimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade RowsLicensedDecember 1, 2000
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Requires Authentication UnlicensedCharacteristics of Arrays of Spray Diffusion FlamesLicensedDecember 1, 2000
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Requires Authentication UnlicensedMaximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade RowLicensedDecember 1, 2000
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Requires Authentication UnlicensedExperimental Evaluation of Precursors to Centrifugal Compressor InstabilityLicensedDecember 1, 2000
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Requires Authentication Unlicensed3-D Inlet Guide Vane Generated Vortical Forcing FunctionsLicensedDecember 1, 2000
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Requires Authentication UnlicensedEffect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip ClearanceLicensedDecember 1, 2000
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Requires Authentication UnlicensedA New Era of Jet Transport Safety By Advanced Legislation?LicensedDecember 1, 2000
