NASA NTRS · 19830000076
Shock Free Airfoil Cascades
Abstract
The CAS22 computer program developed to provide for fast design and analysis of shock free airfoil cascades. CAS22 applicable to aerodynamic analysis and transonic shock free redesign of existing two-dimensional cascades of airfoils. Program is written in FORTRAN IV.
Keep this discovery
Explore connections, maps & timelines
Dulikravich, D. S.. 1983-08-01. Shock Free Airfoil Cascades. https://ntrs.nasa.gov/citations/19830000076
Cite the original work for its findings. Save a collection to share your selection of sources.