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3. Design of a solar UAV for persistent wildlife monitoring

4. Fatigue crack propagation study on the Portuguese Air Force Epsilon TB-30 aircraft

5. Surrogate Modelling of Propeller Noise in Unsteady Load Conditions

6. Analytical and Numerical Analysis of Euler-Bernoulli Beams: Telescopic Beam Deflection

7. Trajectory and aerodynamic analyses of air launched fire-extinguishing projectiles

8. Mission Planning Application Software for Solar Powered UAVs

9. A methodology to develop shallow cracks for qualification of a NDT technique

10. Uso de funções multiquádricas para representação multivariável dos coeficientes aerodinâmicos de perfis alares

11. Importance of periodic CPCP revisions in the evaluation and improvement of the program

12. Preliminary topology optimization of small unmanned aircraft wings for additive manufacturing

13. Mission Planner for Solar Powered Unmanned Aerial Vehicles

14. Automatic engine and propeller selection for mission and performance optimization

15. Sandwich for aeronautical applications

16. Design Optimization for AM of MECSE CubeSat’s Mechanical System

17. Estudo Preliminar da Adaptação da Aeronave Crossover para Voo de Longa Duração a Grande Altitude

18. Analytical Model for the Performance Curves of a Family of Propellers based on Wind Tunnel Tests

19. Design and Analysis of the Mechanical Behaviour of Adhesively-Bonded CFRP T-Joints

20. Structural requirements and launcher validation process for MECSE CubeSat

21. Projeto e caracterização de um material gradiente funcional para escudos térmicos aeroespaciais

22. Mass Prediction Models for Air Cargo Challenge Aircraft

23. Analysis of Slender Aircraft Structures using the Finite Element Method

24. Stress-Strain Relationship Characterization of Armoured Graded Aluminium and Steel Alloys Using a Digital Image Correlation Technique

25. Integration of a Precision Landing System on a Multirotor Vehicle

26. Integrated multi-functional morphing aircraft technologies

27. Preliminary development of an onboard weight and balance estimator for commercial aircraft

28. Design of MECSE Nanosatellite Mechanical Subsystem

29. Investigação e otimização topológica de nervuras obtidas através de fabrico aditivo

30. Mission-Based Multidisciplinary design optimization methodologies for unmanned aerial vehicles with morphing technologies

31. Structuraldesign of a variable span morphing wing: analysis, optimisation and study of the effect of design parameters on its mass

32. Estudo do efeito de ambientes corrosivos em compósitos laminados de carbono-epóxi

33. UrbLog - Prototype 3: Joint System Concept Proposal

34. In-flight thrust measuring system using onboard force transducer

35. Airframe assembly, systems integration and flight testing of a long endurance electric UAV

36. Aerodynamic Analysis of a Forward–Backward Facing Step Pair on the Upper Surface of a Low-Speed Airfoil

37. Estudo e otimização numérica de estrutura para parapente elétrico

38. Efeito da geometria de reparação na resistência ao impacto de compósitos laminados

39. Effect of the Distance Between Impact Point and Hole Position and Non-Perpendicular Holes on the Impact Strength of Composite Laminates

40. Resistência ao Impacto de Juntas Coladas

41. Dimensionamento estrutural de um novo ultraligeiro

42. Estudo do desempenho e otimização aerodinâmica do planador Crossover

43. Projeto estrutural da asa do Crossover

44. Development of the Structure of a long Endurance Electric UAV

45. Quality evaluation of wing sections obtained with different manufacturing techniques

46. Operação de Aeronaves em 'Icing Conditions'

47. Internal Structure of Hybrid Airships Airship Design and Structural Analyses

48. Conceptual Design of the Gondola of a Hybrid Airship Including Loading and Unloading Mechanisms

49. Manufacturing Techniques of a Hybrid Airship Prototype

50. Solar System for a Long Endurance Electric UAV

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