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Delft University of Technology
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Courseware
This course introduces the structural and material design of aircraft. Students will see and understand how aircraft and spacecraft are manufactured, and learn how safety is enshrined at every stage. Experts from the Aerospace Structures and Materials Department of Delft University of Technology will help you explore and analyze the mechanical properties of materials; learning about manufacturing techniques, fatigue, loads and stresses, design considerations and more – all the scientific and engineering principles that structural and materials engineers face on a daily basis.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Space vehicles -- Materials Airplanes -- Materials Aerospace engineering
- Resource Type:
- Courseware
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Courseware
This course provides an overview of and an introduction to the fundamentals of aeronautics, using the history of aviation as a story line. The course uses examples from the very beginning of aviation (the Montgolfier brothers’ balloon flight in 1783 and the Wright brothers’ heavier-than-air flight in 1903) and continues all the way through to the current Airbus A380 and future aircraft. This trajectory will start with a general introduction to aeronautics, to be followed by a closer look at aerodynamics and flight performance.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Aerospace engineering Airplanes Aeronautics Aerodynamics
- Resource Type:
- Courseware
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Courseware
Exploration of space is never out of the news for long and the desire to construct lower-cost, reliable and more capable spacecraft has never been greater. At TU Delft years of technology development and research experience in space engineering allow us to offer this course, which examines spacecraft technologies for satellites and launch vehicles. This course provides: - knowledge of the technical principles of rockets and satellite bus subsystems; - the ability to select state-of-the-art, available components; - analysis of the physical and technical limitations of subsystem components; - identification of the key performance parameters of different spacecraft subsystems; - comparison of the values obtained by ideal theory and real-life ones; - opportunity to make preliminary designs for a spacecraft based on its key requirements. Other spacecraft types, such as interplanetary rovers, are not covered in this course. Spacecraft instrumentation and other payloads are also not covered.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Space vehicles
- Resource Type:
- Courseware
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Courseware
This part of the course Introduction to Aerospace Engineering is focused on two aerospace disciplines: “space and orbital mechanics” and “structures and materials”. These topics are discussed in detail and will provide an understanding for both aircraft and for spacecraft/space missions.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Orbital mechanics Space vehicles -- Materials Airplanes -- Materials Aerospace engineering
- Resource Type:
- Courseware
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Courseware
The following topics are covered: 1. Turning performance (three dimensional equations of motion, coordinate systems, Euler angles, transformation matrices) 2. Airfield performance (take-off and landing) 3. Unsteady climb and descent (including minimum time to climb problem) 4. Cruise flight and transport performance 5. Equations of motion with a wind gradient present 6. Equations of motion applied to various phases of space flight 7. Launch, Vertical flight, delta-V budget, burn out height, staging 8. Gravity perturbations to satellite orbits, J2 effect for low earth orbit satellites, J2,2 effect for Geostationary Earth Orbit sattelites leading to contribution in ï„V budget 9. Patched conics approach for interplanetary flight, gravity assist effect / options for change of excess velocity (2d, 3d), Launch, in orbit insertion.
- Subjects:
- Aeronautical and Aviation Engineering and Mechanical Engineering
- Keywords:
- Aerodynamics Astrodynamics
- Resource Type:
- Courseware
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Courseware
The course is concerned with the concept of structural stability. This concept is applied to discrete and continuous basic structural elements (beams, frames, plates and shells). The fundamental concepts are introduced on the basis of the governing differential equations. The course includes the following topics: - Equations of motion, nonlinear equilibrium equations, stationary potential energy criterion. - Stability analysis for the basic structural elements. - Design methods for stability of basic structural elements.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Buckling (Mechanics) Structural stability
- Resource Type:
- Courseware
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Courseware
Welcome to this course of Aerospace Mechanics of Materials. We are happy that you chose to join us on this exciting journey. This course deals with basic material and geometry dependent analysis of structures. In this course, you will investigate how these material properties, in combination with structural geometries, affect the design and performance of basic structural elements under axial, torsion, bending and shear loading. We have divided this course into eight different subjects and a review chapter. In those subject, you will find video lectures and readings, where the concepts and theory will be explained; examples, where we will solve a problem for you, so you can reinforce the concepts you have learned; and exercises, that will allow you to test your knowledge.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Mechanics Applied Aerospace engineering Mechanical engineering Strength of materials Materials
- Resource Type:
- Courseware
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Courseware
This course is designed to introduce students who wish to specialize in stress analysis of thin-walled structures to more advanced topics such as the analysis of statically indeterminate structures, warping, constraint stresses, shear diffusion, and elements of plate bending.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Airframes Structural analysis (Engineering)
- Resource Type:
- Courseware
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Courseware
This course introduces the basic components of an airframe structure and discusses their use and limitations. The realities of composite design such as the effect of material scatter, environmental knockdowns, and damage knockdowns are discussed and guidelines accounting for these effects and leading to robust designs are presented. The resulting design constraints and predictive tools are applied to real-life design problems in composite structures. A brief revision of lamination theory and failure criteria leads into the development of analytical solutions for typical failure modes for monolithic skins (layup strength, buckling under combined loads and for a variety of boundary conditions) and stiffeners (strength, column buckling under a variety of loads and boundary conditions, local buckling or crippling for one-edge and no-edge-free conditions). These are then combined into stiffened composite structures where additional failure modes such as skin-stiffener separation are considered. Analogous treatment of sandwich skins examines buckling, wrinkling, crimping, intra-cellular buckling failure modes. Once the basic analysis and design techniques have been presented, typical designs (e.g. flange layup, stiffness, taper requirements) are presented and a series of design guidelines (stiffness mismatch minimization, symmetric and balanced layups, 10% rule, etc.) addressing layup and geometry are discussed. On the metal side, the corresponding design practices and analysis methods are presented for the more important failure modes (buckling, crippling) and comparisons to composite designs are made. A design problem is given in the end as an application of the material in this Part of the course.
- Subjects:
- Aeronautical and Aviation Engineering
- Keywords:
- Composite construction Airframes
- Resource Type:
- Courseware