Browse TRAIL Inventories

Two-dimensional compressible flow in centrifugal compressors with straight blades

Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes

Approximate design method for high-solidity blade elements in compressors and turbines

Two-dimensional flow on general surfaces of revolution in turbomachines

Flow surfaces in rotating axial-flow passages

One-dimensional compressible flow in vaneless diffusers of radial- and mixed-flow centrifugal compressors, including effects of friction, heat transfer and area change

Design of two-dimensional channels with prescribed velocity distribution along the channel walls I : relaxation solutions

Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 degrees of turning

Effect of blade-thickness taper on axial-velocity distribution at the leading edge of an entrance rotor-blade row with axial inlet, and the influence of this distribution on alignment of the rotor blade for zero angle of attack

Design of two-dimensional channels with prescribed velocity distributions along the channel walls

Design considerations for mixed-flow centrifugal compressors with high weight-flow rates per unit frontal area


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