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
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- Gauge Lorenz
- Replies: 6
- Forum: Advanced Physics Homework Help
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Why does exhaust velocity stay constant relative to the accelerating rocket?
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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Why does exhaust velocity stay constant relative to the accelerating rocket?
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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Why does exhaust velocity stay constant relative to the accelerating rocket?
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