Force Measurement and Support Integrated Device in Hypersonic Wind Tunnel
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DOI: 10.1109/tim.2021.3129495
Abstract: Airframe/propulsion integrated aerodynamic performance evaluation is one of the key technologies for hypersonic development. Hypersonic aircraft has the characteristics of high flatness ratio which its internal space is fully limited. If the force measurement balance… read more here.
Keywords: wind tunnel; measurement support; integrated device; force ... See more keywords