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- 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
- 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
- Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 degrees of turning
- Design considerations for mixed-flow centrifugal compressors with high weight-flow rates per unit frontal area