Abstract
The results of experimental investigations of thermal-erosion resistance of fiberglass plastic in a supersonic heterogeneous flow, obtained in a ground high-temperature gasdynamic stand, are used to study the resistance of the frontal surface of a hypersonic flying vehicle under conditions of flight in a dusty atmosphere with a velocity of M = 8.
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.
