NASA NTRS · 19660045291
Integral method in compressible laminar boundary layers and its application.
Abstract
Properties of compressible boundary layers with heat transfer and arbitrary pressure gradients calculated, using integral equation and correlation concept for application in hypersonic flows
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Chan, Y.-Y.. 1966-02-01. Integral method in compressible laminar boundary layers and its application.. https://ntrs.nasa.gov/citations/19660045291
Cite the original work for its findings. Save a collection to share your selection of sources.