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pro vyhledávání: '"Alvin Gatto"'
Autor:
Aleksandra Anna Rejniak, Alvin Gatto
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering. 236:1515-1545
ORCID iDs: Aleksandra Anna Rejniak https://orcid.org/0000-0002-2685-2450; Alvin Gatto https://orcid.org/0000-0003-4443-0451. Copyright © The Author(s) 2021. Trailing edge-integrated lobed-mixing geometries are proposed as a viable method for road ve
Autor:
Aleksandra Anna Rejniak, Alvin Gatto
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering. 235:1992-2012
Copyright © IMechE 2020. A new method for supporting ground vehicle wind tunnel models is proposed. The technique employs a centrally mounted sting connecting the front face of the vehicle, adjacent to the floor, to a fixed point further upstream. E
Autor:
Alvin Gatto, Aleksandra Anna Rejniak
Publikováno v:
Flow, Turbulence and Combustion. 106:109-137
New insights into how different ground simulation methods affect road vehicle aerodynamics are presented. Experiments are conducted on a 1/24th-scale model, representative of a Heavy Goods Vehicle, at a Reynolds number, based on width of 2.3 × 105.
Autor:
Alvin Gatto, Mark H Lowenberg
Publikováno v:
Journal of Aircraft. 43:1747-1761
This paper details a quantitative investigation into a cost-effective, three degree-of-freedom test rig to determine aircraft static and dynamic stability derivatives. The technique used a specifically designed three degree-of-freedom gimbaled mechan
Autor:
Alvin Gatto, Sammy Diasinos
Publikováno v:
Mathematical and Computer Modelling.
Publikováno v:
25th AIAA Applied Aerodynamics Conference.
This paper investigates a novel method for the control of ‘morphing’ aircraft. The concept consists of a pair of articulated split wingtips, independently actuated and mounted on a baseline flying wing. The general philosophy behind the concept w
Publikováno v:
24th AIAA Applied Aerodynamics Conference.
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
In this paper an alternative design for variable sweep wings is investigated. It consists of a two-spar, CFRP (carbon fibres reinforced plastics) wing, with truss-like ribs. The spar-web is a shell structure laminated using an unsymmetric stack seque