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Jet Turbine Technology | Plasma | Tribo | TENC | Eco Turbine | Return to Search ListSearch Completed | Title | Fundamentals of Electric Propulsion: Ion and Hall Thrusters
Original File Name Searched: Goebel__cmprsd_opt.pdf | Google It | Yahoo | Bing
Text | Fundamentals of Electric Propulsion: Ion and Hall Thrusters | 493 486 Appendix G bottom cylinder - (vy * r0) vy ^ 2) 'if to 0 12 May + vy ^ 2) * ^ 2 z = z0 + t * vz If (z < lenBottom) Then ' find z when particle hits the rf = rBottom If ((vx ^ 2 + vy ^ 2) * rf ^ 2 < 0#) Then t = (vx * r0) / (vx ^ 2 + sqr arguement is less than 0 then set sqr term 2004 Else t = (vx * r0 + Sqr((vx ^ 2 rf ^ 2 - (vy * r0) ^ 2)) / (vx ^ 2 + vy ^ 2) End If z = z0 End If End If ' end upper If (z < 0#) Then notgone = False End If + vz * t cylinder emission If (z > Length) Then iescape = iescape + 1 vztot = vztot + vz notgone = False End If If (icount > 1000) Then notgone = False icount = 0 nlost = nlost + 1 End If Loop ' while If (maxcount < icount) Next ipart ' particles Range("C11") = (rBottom ^ Range("C12") = maxcount Range("C13") = nlost vz0av = vz0tot / npart Then maxcount = icount 2) * iescape / npart vzav = vztot / iescape DenCor = vz0av / vzav ' Downstream correction factor End Sub ' Clausing | Image | Fundamentals of Electric Propulsion: Ion and Hall Thrusters ![]() |
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