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Aerodynamics field and applications

Shubham yadav

Abstract


This article describes the air intake aerodynamic design for combat aircraft. Axial flow compressor is taken into account. There are explanations for flow distortion, flow stability, and the air intake pressure recovery mass flow need. There are certain design-related issues that are addressed. Comparing air intakes with various designs. For design and analysis, computational numerical techniques are utilised. The study of forces exerted on a solid object, such an aeroplane wing, by a gas (usually air), flowing around it, is known as aerodynamicsSuch a flow can be produced by accelerating air through a stationary object in a wind tunnel or by moving the solid item through the atmosphere. Since the aerodynamic forces are only produced by the motion of the air relative to the object, it is unimportant how the flow was created as long as its velocity and acceleration relative to the object are the same. Because of this, analysing a model with a similar shape placed in a wind tunnel can help us understand the aerodynamic behaviour of an aeroplane during actual flight.


Keywords


Keywords: Aerodynamics, Compressor, Air intake, propulsion, Compatibility

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References


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