Advanced Aircraft Design and Certification I Advanced Aeroelasticity Propulsion Systems Performance and Design It is needed to have a good knowledge, at grade-level, of: Aerodynamics Flight Mechanics

When concluding the course the student must be capable of: - Sizing the aircraft based on its mission and the adequate flying qualities criteria. - Calculating the design structural loads acting on the aircraft, as well as the fatigue conditions. Based on this, to estimate the structural and operational weights. - Knowing the aircraft certification requirements and specifying the means of compliance associated to them, judging their levels of acceptance. - Specifying the means or tests necessary to demonstrate that the aircraft fulfills the certification requirements. - Knowing and specifying and/or designing the subsystems of the aircrafts. - Evaluating the operational costs of the aircraft. - Evaluating the interaction between systems, flying qualities and structural loads, including failure cases. - Knowing the specific design constraints of special aircraft types. - Minimize climate impact of the aircraft by reducing CO2 emisisons

Aircraft Mass and CG Estimation --> Overview, Aircraft Mass Breakdown, Rapid Mass Estimation Method, Semi-empirical Mass Estimation Method, CG and Moments of Inertia. Aircraft Sizing Review --> Wing Design, Wing Control Surfaces, Fuselage and Tails, Quick Mass Sizing and P/L-Range. Powerplant selection and installation --> Engine Types, Thrust Requirements, Integration of Jet Engines, Integration of Propeller Engines, Propeller Analysis. Longitudinal Flying Qualities and HTP design --> Introduction & common A/C tail configurations, HTP main functions, Tail architecture, Basic design guidelines, Longitudinal stability and control, Horizontal tail sizing in preliminary design. Latero-Directional Flying Qualities and VTP design --> VTP main functions & common A/C tail configurations, VTP architecture, Basic design guidelines, Lateral-directional stability and control, Tail sizing in preliminary design. Flight Loads --> General Loads Concepts, Design Envelopes, Balanced NZ manoeuvres, Discrete Gusts, Pitch manoeuvres, Roll manoeuvres, Yaw and OEO manoeuvres. Landing Gear design --> Wheel suspension system, Landing gear retraction, Geometric design criteria, Equivalent single wheel load, Runway classification: LCN/LCG system. Ground Loads --> Ground Loads Conditions, Landing Loads, Ground Handling Loads, Global Effects and Special Cases. Fatigue analysis --> Fatigue concept, Infinite-life, Safe-life, Fail-safe, Damage Tolerant: Accidents that changed aerospace engineering, The fatigue design Philosophy, Fatigue Analysis. Interaction Systems-Flight-Structures --> Aircraft Systems, Flight Control Systems and Flight Control Laws, Analysis of Systems Failures. Introduction to Helicopters. Environmental impact of the aircraft

LEARNING ACTIVITIES AF1 - Theory sessions. AF2 - Problem sessions working individually and in groups. AF3 - Lab sessions in computer rooms. AF5 - Student's Individual work AF6 - Tutorial sessions AF7 - Midterm and final exams METHODOLOGY MD1 - Class lectures by the professor with the support of computer and audiovisual media, in which the main concepts of the subject are developed and the bibliography is provided to complement the students' learning. MD2 - Critical reading of texts recommended by the professor of the subject: press articles, reports, manuals and/or academic articles, either for later discussion in class, or to expand and consolidate the knowledge of the subject. MD3 - Resolution of practical cases, problems, etc. posed by the teacher individually or in groups. MD5 - Preparation of papers and reports individually or in groups.