Abstract
The results of the adiabatic wall temperature measurements of a flat surface placed in a supersonic flow with Mach number M=2.95 are presented. Two flow regimes were investigated. The first is a single-phase flow of dry air, the second is an air-drop stream consisting of a mixture of dry air and finely dispersed water droplets. The presence of droplets in the flow led to the formation of ice sheets on the measured surface, which in turn became the source of shock waves, which caused a strong non-uniformity in the variation of the static pressure and temperature on the measured surface. At this stage, the first data on the rate of cooling of the surface of the adiabatic plate with two flow regimes were obtained.
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 callDisclaimer: 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.
