Automobiles' aerodynamic qualities and how they changed since 1950?
AERODYNAMICS
Aerodynamics is the study
of how gases interact with moving bodies. Because the gas that we encounter
most is air, aerodynamics is primarily
concerned with the forces of drag and lift, which are caused by air passing
over and around solid bodies.
History
of Aerodynamic
As aircraft speed increased, designers began to encounter
challenges associated with air comprehensibility at speeds
near or greater than the speed of sound. The differences in air flows under
such conditions leads to problems in aircraft control, increased drag due to shock waves, and the threat of
structural failure due to aeroelastic flutter.
The ratio of the flow speed to the speed of sound was named
the Mach number after Ernst Mach who was one
of the first to investigate the properties of supersonic flow. William John Macquorn Rankine and Pierre Henri Hugoniot independently developed the theory for flow properties
before and after a shock wave, while Jakob Ackeret led the
initial work of calculating the lift and drag of supersonic airfoils.
This rapid increase in drag led aerodynamicists and aviators to disagree on
whether supersonic flight was achievable until the sound barrier was broken
for the first time in 1947 using the Bell X-1 aircraft.
Fundamental
concepts
Understanding the motion of air around
an object (often called a flow field) enables the calculation of forces
and moments acting on the object. In many
aerodynamics problems, the forces of interest are the fundamental forces of
flight: lift, drag, thrust,
and weight.
Of these, lift and drag are aerodynamic forces, i.e. forces due to air flow
over a solid body.
Calculation of these quantities is often founded upon the assumption that the flow field behaves as a continuum. Continuum flow fields are characterized by properties such as flow velocity, pressure, density, and temperature, which may be functions of position and time. These properties may be directly or indirectly measured in aerodynamics experiments or calculated starting with the equations for conservation of mass, momentum, and energy in air flows. Density, flow velocity, and an additional property, viscosity, are used to classify flow fields.
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