Courses

Courses

International Symposium on Multi-scale Mechanics of Composites

International Symposium on Multi-scale Mechanics of Composites

27-28 October 2022 08:30-12:30 CEST

Syllabus

The symposium “Multi-scale mechanics of composites” aims at outlining the state-of-the-art and the perspectives of the research in the field of multi-scale modelling for advanced composites materials and structures. Scientists and experts will be invited to share their latest research ideas and results in this research direction. This symposium is supported by the International Joint Research Center for Impact Dynamics and Its Engineering Applications, and the Structural Mechanics Behavior Science and Technology Innovation Intelligence Base.

> Download Course Brochure

Participation

You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
You need to Login for registration.

    Courses

    The Space Environment Interaction Engineering: Physics, Test Technology, and Experimental Validation

    The Space Environment Interaction Engineering: Physics, Test Technology, and Experimental Validation

    25 October, 3 and 8 November 2022

    In order to use space for scientific and commercial purposes, it is necessary to understand the Low Earth Orbit (LEO) space environment where most of the activities are now and will be in the future, carried out. LEO environment includes severe hazards such as Atomic Oxygen (AO), Ultraviolet (UV) Radiation, Ionizing Radiation, High Vacuum, Plasma, Micrometeoroids, Debris, Severe Temperature Cycles, and, for some systems, the Re-Entry Environment. It is important to note that these environmental characteristics do simultaneously affect the space systems, materials, and structures, with a remarkable synergistic effect. In order to understand these synergistic effects, whether experimental or theoretical, numerical approaches are of essential importance, as the comprehension of the operative environment becomes a key point to extending the operative life of satellites and structures and withstanding aggressive conditions.

    The course is based on the physics of Space Environment and it is completed with an in-depth analysis of both ground testing methods and the validation of experimental tests according to current regulations given by the major agencies such as ESA and NASA.

    > Download Course Brochure

    Participation

    You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
    You need to Login for registration.

      Courses

      Structural Dynamics and Acoustics of Aerospace and Air Transportation Vehicles

      Structural Dynamics and Acoustics of Aerospace and Air Transportation Vehicles

      29 September 14-18:30 CEST

      This webinar deals with structural dynamics and acoustic design of aerospace and air transportation vehicles. The vibroacoustic response of aerospace and air vehicles is a rather complex phenomenon, which is normally studied considering the dynamics and acoustics of sub-components, such as fuselage sections, wings, flaps, and landing gears, etc. Therefore, the webinar will focus specifically on the vibro-acoustics analysis of elementary mechanical components (e.g. lightweight aluminium framework and panel structures, double-wall structures, composite panels and shells, etc.), from a different point of view (theoretical, numerical and experimental). Several topics will be discussed, such as interior noise mitigation, noise transmission control and vibration attenuation. The physics, design and implementation of both passive vibration attenuation and sound insulation treatments/techniques and active semi-active control systems will be discussed in detail.

      > Download Course Brochure

      Participation

      You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
      You need to Login for registration.

        Courses

        Tethers in Space: deorbiting and power generation

        Tethers in Space: deorbiting and power generation

        27/28 September 10-12 CEST

        The Space Tether consists of a complex structure where there are three main parts: 1) the primary satellite; 2) a secondary
        satellite; 3) a cable (of variable lengths) that is used to join the two spacecraft together. This cable allows the transfer of energy and momentum between the two spacecraft, and this transfer can be present in both directions and, in some cases,
        can switch direction. Space tethers can be classified into two different areas: Passive tethers, which are used simply for mechanical connection and mainly transfer momentum from one part to the other; and Electrodynamic tethers, conductive wires or tapes or more complex structures), in which an electric current can flow and pass from one end to the other. The simplest application involves using the tether system as a de-orbit system; a drag Force is induced on the tether due to its relative motion with respect to the rotating plasma and the satellite.
        An opposite application is the injection of electric current from one satellite which has an effect opposite to the deorbiting;
        this effect can be used to increase the SMA of the system or produce movements in the orbital plane. The Electrodynamic tether is a system that can act as an orbital control for small and relatively big structures (depending on the tether length and on the produced current). Even if the tethers’ dynamics (passive or electrodynamic) are complex and not at all completely understood, the current knowledge in materials and technology is bridging the gap between theory and extensive application in current Space missions.

        > Download Course Brochure

        Participation

        You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
        You need to Login for registration.

          Courses

          High-order accurate numerical methods in aeronautics at the Exascale

          High-order accurate numerical methods in aeronautics at the Exascale

          21/22 September 09-13 CEST

          The aim of this course is to present an overview of high-order accurate numerical methods for mathematical problems that arise in aeronautical and aerospace engineering. Numerical schemes are referred to as high-order accurate when a suitably defined error measure e is a function of the mesh size h as e∼h^p, with p≥3. High-order accuracy is of significant engineering interest in numerical methods because it allows the solution of computational problems with a smaller number of degrees of freedom and higher convergence rates of the error with respect to low-order numerical schemes. The aim of this course is to present an overview of high-order accurate numerical methods for mathematical problems that arise in aeronautical and aerospace engineering. Numerical schemes are referred to as high-order accurate when a suitably defined error measure e is a function of the mesh size h as e∼h^p, with p≥3. High-order accuracy is of significant engineering interest in numerical methods because it allows the solution of computational problems with a smaller number of degrees of freedom and higher convergence rates of the error with respect to low-order numerical schemes.

          > Download Course Brochure

          Participation

          You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
          You need to Login for registration.

            Courses

            Nonlinear spacecraft attitude control

            Nonlinear spacecraft attitude control

            14/15 September 10-12 CEST

            Spacecraft attitude control laws are often designed using linear control design techniques. As a result, their effectiveness
            can be guaranteed only for small attitude angles and small angular velocities since in that situation a linear approximation
            of the attitude equations can be employed. However, there are occasions when the spacecraft motion involves large
            attitude angles and large angular velocities. For those motions, the full nonlinear attitude equations must be used for
            evaluating the effectiveness of attitude control laws. In this course, basic results of Lyapunov stability theory will be
            presented and applied to nonlinear spacecraft attitude control.

            > Download Course Brochure

            Participation

            You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
            You need to Login for registration.

              Courses

              Basics of corrosion and protection of metals for aerospace

              Basics of corrosion and protection of metals for aerospace

              25 July 12-14 CEST, 15:30-17:30 CEST - 26/27 July 11-14 CEST

              Corrosion Control in the aerospace industry is becoming more critical with the aging of the aircraft fleet. In recent years, the aviation industry in terms of corrosion has been undertaken with million pounds. Corrosion control can be one of the aircraft industry’s most effective weapons in the battle against airplane structural failures. Left undetected and/or untreated, corrosion can decrease the load-carrying capacity of primary structures or act as nucleation sites for fatigue or stress corrosion cracks. Thus, corrosion can undermine the integrity of an aircraft and make it unsafe to fly. Therefore, by appropriate selection of materials, maintenance and husbandry, these effects could be decreased.

              > Download Course Brochure

              Participation

              You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
              You need to Login for registration.

                Courses

                Toward Smart Air Mobility: a Model-Based Design Approach

                Toward Smart Air Mobility: a Model-Based Design Approach

                11/12 July 9-12 CEST

                The interest in Urban Air Mobility (UAM) had a steep increase over the last few years. On the one hand, the slow growth rate of ground infrastructures led to critical congestion in urban areas. On the other hand, the increasing demand for moving people and payloads further and faster drove the attention of the research community and stakeholders toward the exploitation of the vertical dimension. With the aim to play a lead role in this new raising market, electrical air platforms with vertical take-off and landing (VTOL) capabilities are being considered key elements for the next generation of controlled airspace. In such a framework, crucial but challenging steps are represented by the optimization of novel configurations and the design of Guidance, Navigation, and Control systems. In this webinar, the fundamentals of the Model-Based Design (MBD) approach will be discussed and applied to VTOL platforms. Attendees will learn the workflow of MBD and investigate the steps required for performance optimization and motion stabilization of rotary-wing vehicles. Test cases will be also presented.

                > Download Course Brochure

                Participation

                You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
                You need to Login for registration.

                  Courses

                  High-speed civil aircraft on-board systems integration

                  High-speed civil aircraft on-board systems integration

                  23 May 9-11 CEST; 25 May 9-11 CEST; 25 May 14:30-16:30 CEST; 26 May 14:30-16:30 CEST

                  High-speed civil aircraft may range from supersonic civil vehicles to hypersonic systems, which can be considered future civil stratospheric passenger or cargo transportations or as the first stage of reusable access to space vehicles. Integration shall be pursued at all levels, systems and subsystems as a key element of success. The webinar will focus on the on-board systems integration of such vehicles. Cryogenic liquid hydrogen is considered a propellant for its potential to extend further the range and its capability to decarbonize the flight. Liquid hydrogen is the core of the multifunctional Thermal and Energy Management System that combines the Fuel System, the Environmental Control System, the Thermal Control and Thermal Protection System, and the Electric Power System. The course will first introduce high-speed vehicles, then the high-speed vehicle on-board systems, highlighting their mutual relationships. Next, main on-board subsystems will be described and sized, and finally, conclusions will be drawn. Students and professionals interested in the high-speed mission and vehicle design can attend the webinar.

                  > Download Course Brochure

                  Participation

                  You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
                  You need to Login for registration.

                    Courses

                    Aerothermodynamic and propulsive investigations to support pollutant and greenhouse gases emissions estimation of future high-speed vehicles

                    Aerothermodynamic and propulsive investigations to support pollutant and greenhouse gases emissions estimation of future high-speed vehicles

                    18 May 2022, 9:00-13:00 CEST

                    The design of a hypersonic civil aircraft flying at stratospheric altitudes is one of the most challenging tasks in modern aerospace due to the high integration needed among the different disciplines. Aerodynamics, propulsion, structures, materials, avionics, onboard subsystems are strictly linked, exchanging each other design requirements and parameters in such a way to fulfil system and mission requirements. The course discloses many of the lessons learned from the activities performed in the framework of the H2020 STRATOFLY project. Specifically, this course is organized into three main parts:

                    • Part 1 (2h: M. Marini and P. Roncioni): Aerodynamic and aerothermodynamic challenges for designing a hypersonic civil transport. Aerodynamic modelling and complete database development from subsonic to hypersonic (Mach 8) speed regimes. The exploitation of aerodynamic databases in mission analysis and trajectory calculation.
                    • Part 2 (1h: G. Saccone): 0D kinetic hydrogen/air combustion modelling and discussion on methodology to evaluate chemical pollutants and GHG emissions released by an Air-Turbo Rocket engine able to operate up to Mach 4.
                    • Part 3 (1h: L. Cutrone): Modelling of a Dual Mode Ramjet able to accelerate a hypersonic vehicle from Mach 4 to Mach 8. Details on modelling techniques for air-intake, isolator, and combustor. Discussion on engine performance and emissions database.

                    > Download Course Brochure

                    Participation

                    You need to buy one of the package list available here and use the Order ID assigned to you after purchase.
                    You need to Login for registration.