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On Jul 15, 3:01*pm, Owen Duffy wrote:
"J.B. Wood" wrote in news:i1monr$2od$1 @ra.nrl.navy.mil: On 07/15/2010 04:14 AM, Owen Duffy wrote: I note some variation in the use of the term 'Radiation Resistance' (Rr) that suggests that it has different meanings to different folk. snip Hello, and I don't find any ambiguities in any of my various EM and antenna theory textbooks. *FWIW, from the IEEE Standard Dictionary of Electrical and Electronics Terms: "Radiation resistance (antenna). The radio of the power radiated by an antenna to the square of the rms antenna current referred to a specified point. *Note: *This term is of limited utility in lossy media." Hmmm. The last statement suggests that, as defined, it is not clear and unambiguous in the real world because the real world involves "lossy media". The "reference to a specified point" suggests that if one gives a value for Rr, it is necessary to also state the reference point. Is that what it means? This is exactly the lack of clarity that is troubling me. So if we're looking at free (in vacuo) space the radiation resistance is simply a "load" resistance component that accounts for where the radiated power goes. *The radiation resistance doesn't include any other resistive losses in the antenna structure/proximity operating environment that may also be dissipating source power introduced at the feedpoint of the antenna. This does not address the issue of ground reflection that I mentioned. *An aerodynamic analogy would be the distinction between "induced" drag (the price paid for "lift") and "parasite" drag, which are both components of the total drag. Sincerely, and 73s from N4GGO, I am not an aerodynamics type, so drawing that analolgy only helps to confuse. You might as well use optics! I know you are trying to be helpful John, but the IREE definition doesn't seem to clarify the issue. To put some numbers on my first example, if I have an NEC model of a centre fed half wave dipole with zero conductor losses, mounted over real (ie lossy) ground, and feedpoint R at resonance is say, 60 ohms, and total power in the *far field* divided by I^2 is say, 50 ohms, is Rr 50 ohms? Is the power "radiated" from such a dipole ONLY the power that makes it to 'distant space', or is radiated power input power less dipole conductor losses? The IREE definition suggests that I need also to state that Rr is 50 ohms at the centre, and the term is is of "limited utility" (not unambiguously clear?) because of the lossy ground reflections. If indeed the term Radiation Resistance is only applicable in lossless scenarios as suggested by the IREE dictionary, what it a clear and unambiguous language for the real world? Cheers Owen In real world terms radiation resistance is measured by the vector that overcomes radiation resistance or the conveyance of communication. This compels the measurement of that which is accelerated as it is an action and reaction type vector. If one doesn't have a measurement of the mass that is being accelerated then radiation resistance itself cannot be supplied. What happens to the accellerated mass has no connection what so ever to the accelleration vector.To find the accelerating vector one must first determine the efficiency of the apparatus used and this will vary dependent on the method used to produce the accelerating vector so that one can determine the losses. So if we cannot identify that vector which creates acceleration of charge where the charge is the measurement of radiation one must first determine what creates radiation so that the radiation unit can be measured. The bottom line is that one must use a superconductor where only the accelerating vector comprises of the impedance seen by the time varying current and where the resistance of the radiating member is divorced from the equation as is coupling losses in the absence of a magnetic field. Art |
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