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 8
... relative velocity , and so rise quicker . It is easier then , to rise against the wind than with the wind behind ; and to alight also , provided the pilot does not descend into a region of relative calm . The aeroplane AA ' is now ...
... relative velocity , and so rise quicker . It is easier then , to rise against the wind than with the wind behind ; and to alight also , provided the pilot does not descend into a region of relative calm . The aeroplane AA ' is now ...
Seite 19
... relative velocity Q , is split along a curved stream line IB , and divides at B on AA ' into the two stream lines BAJ and BA'J ' , where AJ and A'J ' are curved stream lines proceeding from the edge A and A ' . Along AJ and A'J ' the ...
... relative velocity Q , is split along a curved stream line IB , and divides at B on AA ' into the two stream lines BAJ and BA'J ' , where AJ and A'J ' are curved stream lines proceeding from the edge A and A ' . Along AJ and A'J ' the ...
Seite 25
... relative stream as a position of stable equilibrium , seen realised in a falling card or leaf ; and it explains the instability of the axial motion of an elongated body like a ship . The stability of the course of a ship is secured only ...
... relative stream as a position of stable equilibrium , seen realised in a falling card or leaf ; and it explains the instability of the axial motion of an elongated body like a ship . The stability of the course of a ship is secured only ...
Seite 29
... relative bearing of adjacent points is preserved for the two maps z and u , as they may be called ; and there is thus no distortion although there is rotation and change of scale . Conformal representation is then the same problem as ...
... relative bearing of adjacent points is preserved for the two maps z and u , as they may be called ; and there is thus no distortion although there is rotation and change of scale . Conformal representation is then the same problem as ...
Seite 48
... relative to the pilot ; the analytical conditions have been discussed in Lecture I. and II . , and will be found in § 6 of Report 19 . But there is an advantage in extending the theory to a more general case , and beginning as in Report ...
... relative to the pilot ; the analytical conditions have been discussed in Lecture I. and II . , and will be found in § 6 of Report 19 . But there is an advantage in extending the theory to a more general case , and beginning as in Report ...
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00 In Press aeroplane air ship Alternating Current Analysis angular velocity axial axis axle balloon barrier AA bicycle wheel blade Boilers c₁ c₂ calculation Chemistry conformal representation constant cos² couple curve cylinder denotes density Design diagram diameter dynamical Electric Elementary Engineering equation fire balloon flight fluid flying machine formula ft-lb ft² ft³ given gyroscopic Handbook horizontal hydrogen hyperbolic Hyperbolic sector integral Internal Combustion Engines intrinsic equation Kirchhoff Lake Pigments lb/ft² leather lecture lift log Q Machinery Manual Manufacture Mechanical Modern momentum morocco motion motor numbers parallel pendulum pitch polygon Practical precession Railway Report 19 right angles Salter Science Series screw propeller sin² speed spin Steam-engine stream lines theory thrust Treatise Turbine vector velocity Q vertical weight Westminster Series wheel ΦΩ аф
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