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Aerospace Engineering

Some of the elements of aerospace engineering

Aerospace

Aerospace

Fluid mechanics – the study of fluid flow around objects. Specifically aerodynamics concerning the flow of air over bodies such as wings or through objects such as wind tunnels (see also lift aeronautics).
Astrodynamics – the study of orbital mechanics including prediction of orbital elements when given a select few variables. While few schools in the United States teach this at the undergraduate level, several have graduate programs covering this topic (usually in conjunction with the Physics department of said college or university).
Statics Dynamics (engineering mechanics) – the study of movement, forces, moments in mechanical systems.
Mathematics – because aerospace engineering heavily involves mathematics.
Electrotechnology – the study of electronics within engineering.
Propulsion – the energy to move a vehicle through the air (or in outer space) is provided by internal combustion engines, jet engines turbomachinery, or rockets (see also propeller spacecraft propulsion). A more recent addition to this module is electric propulsion ion propulsion.
Control engineering – the study of mathematical modeling of the dynamic behavior of systems designing them, usually using feedback signals, so their dynamic behavior is desirable (stable, without large excursions, with minimum error). This applies to the dynamic behavior of aircraft, spacecraft, propulsion systems, subsystems exist on aerospace vehicles.
Aircraft structures – design of the physical configuration of the craft to withstand the forces encountered during flight. Aerospace engineering aims to keep structures lightweight.
Materials science – related to structures, aerospace engineering also studies the materials of which the aerospace structures are to be built. New materials with very specific properties are invented, or existing ones are modified to improve their performance.
Solid mechanics – Closely related to material science is solid mechanics which deals with stress strain analysis of the components of the vehicle. Nowadays there are several Finite Element programs such as MSC Patran/Nastran which aid engineers in the analytical process.
Aeroelasticity – the interaction of aerodynamic forces structural flexibility, potentially causing flutter, divergence, etc.
Avionics – the design programming of computer systems on board an aircraft or spacecraft the simulation of systems.
Risk reliability – the study of risk reliability assessment techniques the mathematics involved in the quantitative methods.
Noise control – the study of the mechanics of sound transfer.
Flight test – designing executing flight test programs in order to gather analyze performance handling qualities data in order to determine if an aircraft meets its design performance goals certification requirements.
The basis of most of these elements lies in theoretical mathematics, such as fluid dynamics for aerodynamics or the equations of motion for flight dynamics. However, there is also a large empirical component. Historically, this empirical component was derived from testing of scale models prototypes, either in wind tunnels or in the free atmosphere. More recently, advances in computing have enabled the use of computational fluid dynamics to simulate the behavior of fluid, reducing time expense spent on wind-tunnel testing.

Additionally, aerospace engineering addresses the integration of all components constitute an aerospace vehicle (subsystems including power, communications, thermal control, life support, etc.) its life cycle (design, temperature, pressure, radiation, velocity, life time).

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