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
01.10.1983
Sonstige
Keine Angabe
Englisch
Cascades of subharmonic stationary states in strongly non-linear driven planar systems
Online Contents | 2004
|NTIS | 1968
|TIBKAT | 1977
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