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2023-2024 Aeronautical Project Titles
1. Effect of Trailing edge modifications on flow topology and noise emission from wing
2. Numerical optimisation of aerofoils for a high performance low speed aircraft
3. Investigation on the effect of splitter plates to enhance characteristics of flow around cylinder
4. Shock boundary layer interaction studies using CFD
5. Using Lumped vortex element (LVM) method to predict the aerodynamic performance of an aerofoil

6. Design of a high performance swept wing using CFD
7. Effects of leading edge blowing on transonic flow over open cavity
8. Drag reduction of an aircraft afterbody using passive devices – Experimental and numerical studies
9. Experimental studies on mixing in concurrent cold jets
10. Numerical evaluation of flow over blunt body with mass addition in a hypersonic flow
11. Fluid structure interaction studies at wing body junction
12. CFD analysis of thrust vectoring nozzle
13. Load Estimation of a Helicopter blade using CFD
14. CFD studies on flow over wing with and without de-icing

2023-2024 Aeronautical Engineering Projects
Aeronautical Projects
Aeronautics is the science or art involved with the study, design, and manufacturing of air flight capable machines, and the techniques of operating aircraft and
rockets within the atmosphere. The British Royal Aeronautical Society identifies the aspects of "aeronautical Art, Science and Engineering" and "the profession of
Aeronautics (which expression includes Astronautics).
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Later in the beginning 1990s the growing CAA community picked up the term and extensively used it for any kind of numerical method describing the noise radiation
from an aeroacoustic source or the propagation of sound waves in an inhomogeneous flow field. Such numerical methods can be far field integration methods
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While the term originally referred solely to operating the aircraft, it has since been expanded to include technology, business, and other aspects related to
aircraft.The term "aviation" is sometimes used interchangeably with aeronautics, although "aeronautics" includes lighter-than-air craft such as airships, and
includes ballistic vehicles while "aviation" technically does not.
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Attempts to fly without any real aeronautical understanding have been made from the earliest times, typically by constructing wings and jumping from a tower with
crippling or lethal results.
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he modern era of lighter-than-air flight began early in the 17th century with Galileo's experiments in which he showed that air has weight. Around 1650 Cyrano de
Bergerac wrote some fantasy novels in which he described the principle of ascent using a substance (dew) he supposed to be lighter than air, and descending by
releasing a controlled amount of the substance.
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Francesco Lana de Terzi measured the pressure of air at sea level and in 1670 proposed the first scientifically credible lifting medium in the form of hollow metal
spheres from which all the air had been pumped out.
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Charles and the Robert brothers' next balloon, La Caroline, was a Charlière that followed Jean Baptiste Meusnier's proposals for an elongated dirigible balloon, and
was notable for having an outer envelope with the gas contained in a second, inner ballonet. On 19 September 1784, it completed the first flight of over 100 km,
between Paris and Beuvry, despite the man-powered propulsive devices proving useless.
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In an attempt the next year to provide both endurance and controllability, de Rozier developed a balloon having both hot air and hydrogen gas bags, a design which
was soon named after him as the Rozière. The principle was to use the hydrogen section for constant lift and to navigate vertically by heating and allowing to cool
the hot air section, in order to catch the most favourable wind at whatever altitude it was blowing. The balloon envelope was made of goldbeater's skin. The first flight
ended in disaster and the approach has seldom been used since
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Aeroacoustics is a branch of acoustics that studies noise generation via either turbulent fluid motion or aerodynamic forces interacting with surfaces. Noise
generation can also be associated with periodically varying flows. A notable example of this phenomenon is the Aeolian tones produced by wind blowing over fixed
objects.Although no complete scientific theory of the generation of noise by aerodynamic flows has been established, most practical aeroacoustic analysis relies
upon the so-called aeroacoustic analogy
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Lighthill rearranged the Navier–Stokes equations, which govern the flow of a compressible viscous fluid, into an inhomogeneous wave equation, thereby making a
connection between fluid mechanics and acoustics. This is often called "Lighthill's analogy" because it presents a model for the acoustic field that is not, strictly
speaking, based on the physics of flow-induced/generated noise, but rather on the analogy of how they might be represented through the governing equations of a
compressible fluid.
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In their classical text on fluid mechanics, Landau and Lifshitz derive an aeroacoustic equation analogous to Lighthill's (i.e., an equation for sound generated by
"turbulent" fluid motion), but for the incompressible flow of an inviscid fluid. The inhomogeneous wave equation that they obtain is for the pressure p {\displaystyle
p} p rather than for the density ρ {\displaystyle \rho } \rho of the fluid. Furthermore, unlike Lighthill's equation, Landau and Lifshitz's equation is not exact; it is an
approximation.
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These would be lighter than the displaced air and able to lift an airship. His proposed methods of controlling height are still in use today; by carrying ballast which
may be dropped overboard to gain height, and by venting the lifting containers to lose height. In practice de Terzi's spheres would have collapsed under air
pressure, and further developments had to wait for more practicable lifting gases.
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A rocket or rocket vehicle is a missile, spacecraft, aircraft or other vehicle which obtains thrust from a rocket engine. In all rockets, the exhaust is formed entirely from
propellants carried within the rocket before use. Rocket engines work by action and reaction. Rocket engines push rockets forwards simply by throwing their
exhaust backwards extremely fast.
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Chemical rockets are the most common type of rocket and they typically create their exhaust by the combustion of rocket propellant. Chemical rockets store a large
amount of energy in an easily released form, and can be very dangerous. However, careful design, testing, construction and use minimizes risks.
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The aircraft design process is the engineering design process by which aircraft are designed. These depend on many factors such as customer and manufacturer
demand, safety protocols, physical and economic constraints etc. For some types of aircraft the design process is regulated by national airworthiness authorities.
This article deals with powered aircraft such as airplanes and helicopter designs.
Final Year projects for Aeronautical Engineering Students
Later in a publication 1986[2] the same authors introduced the abbreviation CAA. The term was initially used for a low Mach number approach (Expansion of the
acoustic perturbation field about an incompressible flow) as it is described under EIF.
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