Philosophical MagazineTaylor & Francis., 1919 - Physics |
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Page 4
... given by дро ∞ a = √ 9 de dz = -9√ " { 3 = ( pu ) + 3y ( pe ) + 2 = ( p10 ) } dz , ( 7 ) at = √ at 0 by the equation of continuity . ду Now pw is zero when z = 0 and when z is infinite , since there is no vertical velocity on the ...
... given by дро ∞ a = √ 9 de dz = -9√ " { 3 = ( pu ) + 3y ( pe ) + 2 = ( p10 ) } dz , ( 7 ) at = √ at 0 by the equation of continuity . ду Now pw is zero when z = 0 and when z is infinite , since there is no vertical velocity on the ...
Page 7
... given by ӘР at HB DR Sw3Po dy Now if the disturbance is travelling unaltered we must have a a at + U + V a дӕ ду = 0 , where U and V are the components of the velocity of trans- lation , and the object of the operation is any of the ...
... given by ӘР at HB DR Sw3Po dy Now if the disturbance is travelling unaltered we must have a a at + U + V a дӕ ду = 0 , where U and V are the components of the velocity of trans- lation , and the object of the operation is any of the ...
Page 12
... given by do dI ds 1 -- cos $ ) . + 2√ / s sin $ 10 = 0 .. · ( 2 ) = de de Since dode = 4k0 ( y + a0 ) + 2k02a , and contains the factor 2π / λ , it will be large , so that the first term in equation ( 2 ) is negligible . That equation ...
... given by do dI ds 1 -- cos $ ) . + 2√ / s sin $ 10 = 0 .. · ( 2 ) = de de Since dode = 4k0 ( y + a0 ) + 2k02a , and contains the factor 2π / λ , it will be large , so that the first term in equation ( 2 ) is negligible . That equation ...
Page 15
... given by Imax . = ( 1 + √ / S ) 2 Imin . = ( 1 - V / S ) ! " ( 13 ) where S is given by equation ( 8 ) . The intensity - curve for a plane 5 mm . behind the edge is shown in fig . 2 ( c ) . It will be seen that the ratio of the minima ...
... given by Imax . = ( 1 + √ / S ) 2 Imin . = ( 1 - V / S ) ! " ( 13 ) where S is given by equation ( 8 ) . The intensity - curve for a plane 5 mm . behind the edge is shown in fig . 2 ( c ) . It will be seen that the ratio of the minima ...
Page 18
... ( 4 ) we get x = ηλ a02 20 2 ( 15 ) which gives the abscissæ of the points at which the loci cut the straight lines const . The ordinates of these points . = are given by 3 20 = -5a ηλ 402 so 18 Mr. T. K. Chinmayam on the Flow of.
... ( 4 ) we get x = ηλ a02 20 2 ( 15 ) which gives the abscissæ of the points at which the loci cut the straight lines const . The ordinates of these points . = are given by 3 20 = -5a ηλ 402 so 18 Mr. T. K. Chinmayam on the Flow of.
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absorption coefficient æther amplitude angle aperture assumption atomic number axis boundary C₁ calculated centre circuit collision components constant corresponding curve cylinder damping deflexion density determined diffraction distance effect electric elements energy equal equation experimental experiments expression force formula frequency give given H atoms hydrogen increase integral intensity ionization ionization potential J. J. Thomson L-systems light Lord Rayleigh luminosity magnetic field maxima and minima maximum method minima molecules motion nucleus number of electrons number of H number of scintillations observed obtained oscillations paper particles peak potential Phil plane plate positive pressure primary quadratic form quant-number radiation radium radius range rays recombination reflexion resonance potential ring screen secondary speed surface Table temperature thallium theory tube values vapour velocity vibrations volts wave-length zero