NASA Technical Reports Server (NTRS) 19820008171: CAS22 - FORTRAN program for fast design and analysis of shock-free airfoil cascades using fictitious-gas conceptReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820008171: CAS22 - FORTRAN program for fast design and analysis of shock-free airfoil cascades using fictitious-gas concept


NASA Technical Reports Server (NTRS) 19820008171: CAS22 - FORTRAN program for fast design and analysis of shock-free airfoil cascades using fictitious-gas concept - Download this document for free, or read online. Document in PDF available to download.

Download or read this book online for free in PDF: NASA Technical Reports Server (NTRS) 19820008171: CAS22 - FORTRAN program for fast design and analysis of shock-free airfoil cascades using fictitious-gas concept
A user-oriented computer program, CAS22, was developed that is applicable to aerodynamic analysis and transonic shock-free redesign of existing two-dimensional cascades of airfoils. This FORTRAN program can be used: (1) as an analysis code for full-potential, transonic, shocked or shock-free cascade flows; (2) as a design code for shock-free cascad

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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