Abstract
The results of studies of heat fluxes that can occur in the gas supersonic flow created in the wind tunnel with a magnetogasdynamic accelerator are presented. For two operation modes of the installation, measurements of heat fluxes to the surface of a calorimetric model were performed. The dependences of these parameters on induction of magnetic field on axis of the MHD accelerator were obtained for the first time. It was found that their values reached a level of 6 MW/m2. The experimental data were compared with the results of a numerical simulation of a longitudinal flow past cylinder with a flat face in the real conditions of the wind tunnel, that allowed to calculate other characteristics of the gas flow. As a result, it is shown that this setup is enabled to create high-speed gas flows with high enthalpy that can be used in the development of prospective hypersonic aircrafts.
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.
