E. Houghton, P. Carpenter's Aerodynamics for Engineering Students PDF

By E. Houghton, P. Carpenter

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The result is a symmetrical shape, called the thickness distribution or symmetrical fairing. An important parameter of the thickness distribution is the maximum thickness, or depth, t . This, when expressed as a fraction of the chord, is called the thickness/ chord ratio. It is commonly expressed as a percentage 100t/c%. Current values in use range from 13% to 18% for subsonic aircraft down to 3% or so for supersonic aircraft. The position along the chord at which this maximum thickness occurs is another important parameter of the thickness distribution.

369 which was also published in the Journal of the Royal Aeronautical Society, November 1958. 36 Aerodynamics for Engineering Students (a) Fig. 13 (a) The displacement thickness of the boundary layer (hatched area) represents an effective change to the shape of the aerofoil. ) (b) Pressure-distribution on an aerofoil section in viscous flow (dotted line) and inviscid flow (full line) total temperature in the boundary layers. But these definitions are rather unhelpful for giving a clear idea of the physical nature and mechanisms behind form drag, so a simple explanation is attempted below.

369 which was also published in the Journal of the Royal Aeronautical Society, November 1958. 36 Aerodynamics for Engineering Students (a) Fig. 13 (a) The displacement thickness of the boundary layer (hatched area) represents an effective change to the shape of the aerofoil. ) (b) Pressure-distribution on an aerofoil section in viscous flow (dotted line) and inviscid flow (full line) total temperature in the boundary layers. But these definitions are rather unhelpful for giving a clear idea of the physical nature and mechanisms behind form drag, so a simple explanation is attempted below.

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Aerodynamics for Engineering Students by E. Houghton, P. Carpenter


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