Issue
Licensed
Unlicensed
Requires Authentication
Volume 7, Issue 3-4
Contents
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Requires Authentication UnlicensedCONTENTSLicensedDecember 1, 1990
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Requires Authentication UnlicensedUse of Holography in Vibration and Flutter Study of FansLicensedDecember 1, 1990
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Requires Authentication UnlicensedLinear State Variable Dynamic Model and Estimator Design for Allison T406 Gas Turbine EngineLicensedDecember 1, 1990
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Requires Authentication UnlicensedLife Enhancement of a Gas Turbine Engine by Temperature ControlLicensedDecember 1, 1990
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Requires Authentication UnlicensedTurbomachinery Alloys Affected by Solid ParticlesLicensedDecember 1, 1990
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Requires Authentication UnlicensedAnalysis and Matching of Gas Turbine ComponentsLicensedDecember 1, 1990
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Requires Authentication UnlicensedTheoretical Investigation of the Interaction Between a Compressor and the Components During SurgeLicensedDecember 1, 1990
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Requires Authentication UnlicensedCorrelations for Prediction of Discharge Rate, Core Angle and Air Core Diameter of Swirl Spray AtomizersLicensedDecember 1, 1990
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Requires Authentication UnlicensedLDA Measurement of the Passage Flow Field in an Annular Airfoil CascadeLicensedDecember 1, 1990
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Requires Authentication UnlicensedNumerical Solution to Transonic Potential Equations on S2 Stream Surface in a TurbomachineLicensedDecember 1, 1990
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Requires Authentication UnlicensedA Unified Method for Solving Aerodynamic Cascade Design Problems on an Arbitrary Surface of RevolutionLicensedDecember 1, 1990
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Requires Authentication UnlicensedSemi-Constant Volume Pulse Combustion for Gas Turbine Engine StartingLicensedDecember 1, 1990
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Requires Authentication UnlicensedExperiment on the Effects of Vortex Generators upon the Flat Plate Boundary LayersLicensedDecember 1, 1990
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Requires Authentication UnlicensedA Review of Friction Damping of Turbine Blade VibrationLicensedDecember 1, 1990
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Requires Authentication UnlicensedHypersonic Inlet Oblique Shock Interaction with a Laminar Boundary LayerLicensedDecember 1, 1990
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Requires Authentication UnlicensedCathode and Insulator Materials for a 30 kW Arcjet ThrusterLicensedDecember 1, 1990
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Requires Authentication UnlicensedImproving the Development Process for Main Combustor Exit Temperature DistributionLicensedDecember 1, 1990
