Computer Program for Relaxation Solutions of the Nonlinear Small-Disturbance Equations for Transonic Flow in an Axial Compressor Blade Row.
Interim scientific rept.,
CALSPAN CORP BUFFALO N Y
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This report contains a description of a computer program for calculating the three-dimensional transonic flow through a compressor blade row, in the nonlinear small-disturbance approximation, and for subsonic values of the inlet relative Mach number at the blade tip. The problem formulation is reviewed briefly following this, a description of the program is given together with a listing and sample case. Author
- Hydraulic and Pneumatic Equipment
- Fluid Mechanics