Plane cascade flow solved using improved surface-singularity methods. Current external aerodynamic integral-equation techniques adapted for use in internal flow calculation. Inherent computational speed and flexibility of integral equation solutions make them useful for design calculations.
PANEL Code for Planar Cascades
NASA Tech Briefs ; 7 , 4
1983-10-01
Miscellaneous
No indication
English
Cascades of subharmonic stationary states in strongly non-linear driven planar systems
Online Contents | 2004
|NTIS | 1968
|TIBKAT | 1977
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