Experimental and numerical investigations of unsteady aerodynamic derivatives for a generic lambda wing UCAV configuration
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DOI: 10.1007/s13272-019-00426-w
Abstract: Experimental and numerical investigations have been conducted to analyze the unsteady aerodynamic and flight mechanical behavior of a 53° flying wing configuration representing a generic unmanned combat air vehicle (UCAV). The considered vehicle is named… read more here.
Keywords: numerical investigations; ucav configuration; unsteady aerodynamic; wind tunnel ... See more keywords