Abstract
A hypersonic viscous flow in the shock layer near sharp cones is considered. The profiles of density and velocity, the slopes of the shock wave, and the pressures and heat fluxes calculated on the basis of the full viscous shock layer equations are compared with available experimental and theoretical data.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callMore From: Journal of Applied Mechanics and Technical Physics
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
