The Dynamics of Mechanical Flight: Lectures Delivered at the Imperial College of Science and Technology, March, 1910 and 1911Constable, 1912 - 121 Seiten Lærebogsagtig redegørelse for teori og beregninger vedr. aerodynamik og flyvning. |
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Seite 14
... stream lines of liquid through an orifice or past a barrier , and of the discontinuity arising at an edge . This theory will represent the substance of these Lectures ; but we may lead up to it through the ancient assumption of Newton ...
... stream lines of liquid through an orifice or past a barrier , and of the discontinuity arising at an edge . This theory will represent the substance of these Lectures ; but we may lead up to it through the ancient assumption of Newton ...
Seite 19
... stream lines , AJ and A'J ' , as they leave an edge , A and A ' , of the barrier AA ' . These are not straight and in the line AA ' , as in Newton's theory , but curved backward , as in Fig . 4 , forming a skin or bounding surface ...
... stream lines , AJ and A'J ' , as they leave an edge , A and A ' , of the barrier AA ' . These are not straight and in the line AA ' , as in Newton's theory , but curved backward , as in Fig . 4 , forming a skin or bounding surface ...
Seite 32
... lines on the right hand . The same argument as in ( 3 ) applies to each of ... streaming motion we do not consider the z = x + yi polygon , as in the Electrical Applications given in J. J. ... stream 32 THE DYNAMICS OF MECHANICAL FLIGHT.
... lines on the right hand . The same argument as in ( 3 ) applies to each of ... streaming motion we do not consider the z = x + yi polygon , as in the Electrical Applications given in J. J. ... stream 32 THE DYNAMICS OF MECHANICAL FLIGHT.
Seite 33
... stream lines , over which y is constant , and represented by parallel lines in the w diagram , and the angle a in the w polygon is either + ( 18 ) dw du = product of factors of the form ( u - or , so that - 1 a ) or ( u - b ) +1 which ...
... stream lines , over which y is constant , and represented by parallel lines in the w diagram , and the angle a in the w polygon is either + ( 18 ) dw du = product of factors of the form ( u - or , so that - 1 a ) or ( u - b ) +1 which ...
Seite 40
... stream lines in Fig . 12 . The pressure in rear of the plane in its wake is taken as atmospheric , up to and along the skin of the bounding stream AJ and A'J ' , the air behind being at rest relatively to AA ' , or in a state of ...
... stream lines in Fig . 12 . The pressure in rear of the plane in its wake is taken as atmospheric , up to and along the skin of the bounding stream AJ and A'J ' , the air behind being at rest relatively to AA ' , or in a state of ...
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