Browse TRAIL Inventories

Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors

Formulas and Tables of Coefficients for Numerical Differentiation With Function Values Given at Unequally Spaced Points and Application to Solution of Partial Differential Equations

A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution

Method of analysis for compressible flow arbitrary turbomachine blades on general surface of revolution

A method of solving the direct and inverse problem of supersonic flow along arbitrary stream filaments of revolution in turbomachines

A General Through-Flow Theory of Fluid Flow With Subsonic or Supersonic Velocity in Turbomachines of Arbitrary Hub and Casing Shapes

Survey of Available Information on Internal Flow Losses Through Axial Turbomachines

An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

Analysis of flow in a subsonic mixed-flow impeller

A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial-, Radial-, and Mixed-Flow Types

Matrix and Relaxation Solutions That Determine Subsonic Through Flow in an Axial-Flow Gas Turbine

Subsonic Flow of Air Through a Single-Stage and a Seven-Stage Compressor


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