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- Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design
- Application of Radial-Equilibrium Condition to Axial-Flow Compressor and Turbine Design
- 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