Recent content by adphysics
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Why Can We Freely Choose the Divergence of A in Electromagnetic Theory?
I know. I'm just having trouble understanding how, say, the Lorenz gauge is actually related to the simultaneous gauge transforms shown above. In all the derivations I've encountered of the wave equations for E and B using the Lorenz gauge, like this one...- adphysics
- Post #5
- Forum: Advanced Physics Homework Help
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Why Can We Freely Choose the Divergence of A in Electromagnetic Theory?
Sorry, I should have been more clear. That part I understand. I understand why, if we begin with E=-grad(phi)-dA/dt and make the simultaneous gauge transforms, we have the same electric field. What I don't understand is the following: Take the divergence of the electric field: div...- adphysics
- Post #3
- Forum: Advanced Physics Homework Help
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Why Can We Freely Choose the Divergence of A in Electromagnetic Theory?
I understand the concept of a gauge transform, and I understand why it is that the magnetic field would be unchanged with the addition of the gradient of an arbitrary scalar potential onto the magnetic vector potential A, and I understand why the electric field E would be invariant under the...- adphysics
- Thread
- Gauge Lorenz
- Replies: 6
- Forum: Advanced Physics Homework Help
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The Rocket Equation: Unraveling the Mystery
Oh, yeah. The engine is on the back of the rocket, so it accelerates with the rocket, so if an engine ejects exhaust at a velocity v, then this is what is observed from the rocket's point of view. Now I feel somewhat embarrassed, but at least the rocket equation makes sense now.- adphysics
- Post #5
- Forum: Advanced Physics Homework Help
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The Rocket Equation: Unraveling the Mystery
Oops. So assuming a constant mass flow rate the propellant exerts a constant force on the rocket so the rocket's acceleration increases as follows: a(t)=F[1/m(t)] where F is a constant (until fuel runs out) where m(t) is the mass of the rocket at time t. m(t)=m(initial)-bt where b is a...- adphysics
- Post #3
- Forum: Advanced Physics Homework Help
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The Rocket Equation: Unraveling the Mystery
In deriving the rocket equation, there is one part I don't understand. The velocity of exhaust with respect to the body is assumed to be constant, where: v(exhaust wrt body)=v(exhaust wrt inertial)-v(body wrt inertial) So assuming a constant mass flow rate, the rocket propellant exerts a...- adphysics
- Thread
- Rocket Rocket equation
- Replies: 5
- Forum: Advanced Physics Homework Help