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Aerodynamic Testing of Helicopter Novel Air Intakes (ATHENAI)
Date du début: 1 sept. 2013, Date de fin: 31 août 2015,
The project is aimed on enhancing the aerodynamic performance of novel engine air intake concepts for helicopters by shape optimization. Comprehensive wind tunnel tests are performed on a full scale model of a helicopter fuselage section comprising engine cowling and air intake flow passages. The main effort is on two wind tunnel campaigns to analyze in detail the aerodynamic characteristics of th ...
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