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Integration over these velocity space variables would then take the form de [d³on(r, v.1)= [ do v² ²*do* do sin On(r,v,,1) - de fdân(r. E.Â.1) S²º° dE where we have identified the differential solid angle dŷ = sin 0d0 do. One

Integration over these velocity space variables would then take the form de [d³on(r, v.1)= [ do v² ²*do* do sin On(r,v,,1) - de fdân(r. E.Â.1) S²º° dE where we have identified the differential solid angle dŷ = sin 0d0 do. One

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Integration over these velocity space variables would then take the form [d³on(r, v.1)= [ do v² ²*do* dð sin On(r,v,,1) dE de - de fdân(r. E.Â.1) where we have identified the differential solid angle dŵ = sin 0d0 do. One
Transcribed Image Text:Integration over these velocity space variables would then take the form [d³on(r, v.1)= [ do v² ²*do* dð sin On(r,v,,1) dE de - de fdân(r. E.Â.1) where we have identified the differential solid angle dŵ = sin 0d0 do. One
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