Issue
Licensed
Unlicensed
Requires Authentication
Volume 17, Issue 1
Contents
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Requires Authentication UnlicensedCONTENTSLicensedMarch 1, 2000
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Requires Authentication UnlicensedFailure Mode of Thermal Barrier Coatings for Gas Turbine Vanes Under BendingLicensedMarch 1, 2000
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Requires Authentication UnlicensedAeroacoustic Characteristics of Notched Circular-Slot JetsLicensedMarch 1, 2000
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Requires Authentication UnlicensedAeroacoustic Characteristics of Notched 2:1 Elliptic-Slot JetsLicensedMarch 1, 2000
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Requires Authentication UnlicensedSolution of Shock with Variable Specific Heat and its Application in Hypersonic InletLicensedMarch 1, 2000
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Requires Authentication UnlicensedReview: Recent Investigations on Tip Clearance Flows in Centrifugal CompressorsLicensedMarch 1, 2000
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Requires Authentication UnlicensedCalculation of Swirling Recirculating Turbulent Flow Using a Two-Layer ApproachLicensedMarch 1, 2000
