NASA Technical Reports Server (NTRS) 19950010173: FPCAS2D user-s guide, version 1.0Report as inadecuate




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The FPCAS2D computer code has been developed for aeroelastic stability analysis of bladed disks such as those in fans, compressors, turbines, propellers, or propfans. The aerodynamic analysis used in this code is based on the unsteady two-dimensional full potential equation which is solved for a cascade of blades. The structural analysis is based o

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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