Universidad Carlos III de Madrid

Aeroelasticity

251-15355

Iowa State Course Substitution

Advanced Flight Structures

AER E 421

Course Info
International Credits:
3.0
Converted Credits:
2.0
Semester:
fall
Country:
Spain
Language:
English
Course Description:
Aeroelasticity & Dynamic Loads. Getting Started. - Aeroelasticity as a multidisciplinary task - Normal modes at a glance - Stability problems vs. Response problems - Basic flutter mechanisms. CS25.629 2D Aeroelasticity: fixing concepts with some analytical 2D solutions - The ¾ span aerofoil. Pitch and plunge modes. - Revisiting steady aerodynamics. The standard atmosphere. - Introduction to 2D unsteady aerodynamics. Wagner, Küssner, Theodorsen. - Solution of the 2D aeroelastic equation. - Sensitivity to Xcg. 2D & 3D Static aeroelasticity: divergence and control reversal - Static aeroelasticity of a 2D rigid aerofoil. - Static aeroelasticity of a fixed wing - Divergence. Effect of sweep angle on divergence speed. - Control effectiveness. Effect of wing flexibility on control effectiveness. 3D Aeroelasticity: The structural model & the normal modes - Revisiting 1 d.o.f system. - Multiple d.o.f. systems - The Finite Element Method (FEM) for structural analysis. - From stick models to full FEM models. The stiffness matrix. - Mass models. The mass matrix. - Condensation. - Structural Normal modes. Frequencies and mode shapes. The experimental modal analysis and the GVT. Dynamic model validation. - Ground Vibration Test (GVT) description. - Introduction to Digital Signal Processing (DSP). The Fast Fourier Transform (FFT). - Experimental Modal Analysis. - Comparison between test and simulations. MAC. - Updating FEM model to match GVT results. 3D Aeroelasticity: unsteady aerodynamics, origins (Wagner, Küssner, Theodorsen). Rodden and the Doublet Lattice Method (DLM) - Continuing with 2D unsteady aerodynamics. - The Finite Element Method (FEM) for aerodynamic analysis. - Rodden and the Doublet lattice Method - Aerodynamic corrections to match wind tunnel or flight tests. The flutter equation and its solution (natural aircraft) - Derivation of flutter equation from Lagrange equations. - Complex matrix eigenvalues & eigenvector solution. - Evolution of modal frequency and modal damping with flight speed. - The V-g plot unveiled - Physical description of classical lifting surface flutter mechanisms - Airworthiness regulations CS25.629 (and the evolution from FAR 25.629 and JAR 25.629) Flutter speed sensitivities. Control surface massbalance. Aeroservoelasticity (coupling with Flight Control System laws) - Sensitivity analyses: mass configuration, Mach number, control surface aerodynamic hinge moment, etc. - Physical description of classical control surface flutter mechanisms. - Sensitivity to control surface mass balance. - Covering uncertainties & addressing failure cases (structural single failures, damage tolerance, water ingress, composite delaminations...) - Revisiting aircraft controls. Introduction to aircraft flight control system laws. - Aeroservoelasticity. - Physical description of most common aeroservoelastic couplings. Flight Flutter Test. Aeroelastic model validation. Wrap up of aeroelastic stability problems. - Flight Flutter Test (FVT) description. - Aircraft response to control surface sweeps and pulses. - Revisiting Digital Signal Processing (DSP). Noise treatment. Averaging. Windowing. Aliasing. Leakage,... - Experimental Modal Analysis applied to Flight Test. - Comparison between flight test and simulations. Scatter. - Wrap up of aeroelastic stability problems. The concept of loads. Monitoring stations. Checkstress loads and fatigue loads. Dynamic loads and why they are different form static loads. Structural response to transient excitation. - What is fast and what is slow - Direct response vs. Modal response - Frequency domain response - Time domain response Ground dynamic loads: dynamic landing & Taxi - Relevance

Review

Evaluation Date:
March 25, 2016
Evaluated:
Liming Xiong
Comments:
This course can be used as a substitute for AER E 421