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View article: Design and Validation of a New Morphing Camber System by Testing in the Price—Païdoussis Subsonic Wind Tunnel
Design and Validation of a New Morphing Camber System by Testing in the Price—Païdoussis Subsonic Wind Tunnel Open
This paper presents the design and wind tunnel testing of a morphing camber system and an estimation of performances on an unmanned aerial vehicle. The morphing camber system is a combination of two subsystems: the morphing trailing edge a…
View article: Aerodynamic Modelling of Unmanned Aerial System through Nonlinear Vortex Lattice Method, Computational Fluid Dynamics and Experimental Validation - Application to the UAS-S45 Bàlaam: Part 1.
Aerodynamic Modelling of Unmanned Aerial System through Nonlinear Vortex Lattice Method, Computational Fluid Dynamics and Experimental Validation - Application to the UAS-S45 Bàlaam: Part 1. Open
This paper describes a methodology to predict the aerodynamic behaviour of an Unmanned Aerial System. Aircraft design and flight dynamics modelling are mainly concerned with aerodynamics, and thus its estimation requires a high level of ac…
View article: Design, Manufacturing, and Testing of a New Concept for a Morphing Leading Edge using a Subsonic Blow Down Wind Tunnel
Design, Manufacturing, and Testing of a New Concept for a Morphing Leading Edge using a Subsonic Blow Down Wind Tunnel Open
This paper presents the design and wind tunnel test results of a wing including a morphing leading edge for a medium unmanned aerial vehicle with a maximum wingspan of 5 m. The design of the morphing leading edge system is part of research…
View article: Experimental validation of a new morphing trailing edge system using Price – Païdoussis wind tunnel tests
Experimental validation of a new morphing trailing edge system using Price – Païdoussis wind tunnel tests Open
This paper presents the design and manufacturing of a new morphing wing system carried out at the Laboratory of Applied Research in Active Controls, Avionics and AeroServoElasticity (LARCASE) at the ETS in Montréal. This first version of a…
View article: Measuring Impact of an Aileron on Aerodynamic Behaviour in a Wind Tunnel
Measuring Impact of an Aileron on Aerodynamic Behaviour in a Wind Tunnel Open
Ailerons are one factor that impacts a wing’s aerodynamic behaviour, fuel consumption and carbon dioxide emissions. In order to evaluate their impact on the aerodynamic behaviour of a wing, wind tunnel tests were carried out at different s…
View article: Automating Wing Angle Changes inside the LARCASE Price – Païdoussis Wind Tunnel
Automating Wing Angle Changes inside the LARCASE Price – Païdoussis Wind Tunnel Open
Student researchers at ÉTS designed an aerodynamic balance to automatically rotate parts of their reduced scale models at precise angles inside a wind tunnel in order to calculate lift, drag and moment coefficients. This aerodynamic balanc…