Programs for computation of velocities and stream-lines on a blade-to-blade surface of a turbomachine.
Finite difference method computer programs for calculation of velocities and streamlines on blade to blade surface of revolution of turbomachine
Engineering topics
Publications and source records attributed to Katsanis, T..
Finite difference method computer programs for calculation of velocities and streamlines on blade to blade surface of revolution of turbomachine
FORTRAN computer program for spline fit curve with function valves
Finite difference method for symmetric positive linear differential equations, discussing methods to solve finite difference equations generated
Neumann problem solution for curved boundaries, using quasi-orthogonals instead of normals to streamlines
Computer program calculates the velocity distribution and streamlines over widely separated blades of turbomachines. It gives the solutions of a two dimensional, subsonic, compressible nonviscous flow problem for a rotating or stationary circular cascade of blades on a blade-to-blade surface of revolution.
FORTRAN computer program for calculating two dimensional subsonic inviscid flow for rotating or stationary circular cascade of blades on blade to blade stream surface of turbomachine
Finite difference method for solving symmetric positive linear differential equations
Quasi three-dimensional compressible flow analysis to determine aerodynamic velocity distribution on turbine blades
NASA radial flow turbine research related to Brayton cycle power generator, investigating size, Reynolds number and speed effects on efficiency and flow
Fortran computer program for calculating velocities and streamlines for two-dimensional incompressible flow in axial blade rows
Radial flow turbines as related to Brayton cycle space power systems
Computer program based on an equation for the velocity gradient along an arbitrary quasi- orthogonal analyzes flow through a turbomachine. The program obtains meridional solutions for a hub-to-shroud analysis and blade-to-blade analysis at the hub, mean, and shroud surfaces in a single computer run.
Arbitrary quasi-orthogonals for calculating flow distribution in turbomachine, noting digital computer calculations
Quasi-three-dimensional compressible flow analysis for calculating blade surface velocities for axial flow turbine blade
Arbitrary quasi-orthogonals for calculating flow distribution in turbomachine, noting digital computer calculations
Turbomachine blade surface flow distribution analysis by arbitrary quasi-orthogonals - radial inflow turbine Fortran computer program
Fortran computer program for calculating flow in radial inflow gas turbine
Arbitrary quasi-orthagonal method for calculating flow distribution in turbomachine suitable for computer programming