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Velocities after off center collision

  1. Jan 30, 2013 #1
    Hi, I just have a quick question I hope I can explain well.

    Suppose you have a metal rod that you apply a force to for a brief moment at the center of mass. It won't rotate and it will move forward at velocity V. Now you reset the scene and move the the force so it's applied off center off the mass, it will then also provide angular velocity. I'm guessing the rod's linear velocity would now be less, since some of the energy has gone into the rotation. Am I right? and if this is true, how do you go about working out the angular and linear components?
     
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  3. Jan 30, 2013 #2

    mfb

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    Edit: Depends on the setup.
    Conservation of linear and angular momentum
     
    Last edited: Jan 30, 2013
  4. Jan 30, 2013 #3
    But how would conservation of momentum equations change? Since I'd do a conservation of momentum for linear, then for angular, but that won't change the outcome of the linear, only the angular.

    I'm writing a small program, and I'm adding all forces and torques together before applying the accelerations, and the steps are as follows:

    - Work out Force tail plane exerts on plane

    - Linear Acceleration = Force/Mass

    - Torque = crossproduct of Force and distance from center of mass.

    But this method yields the same linear acceleration as if the tail plane were placed on the CG.

    What am I doing wrong?
     
  5. Jan 30, 2013 #4

    mfb

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    You are right, the linear velocity depends on the setup:
    - If you hit your rod with another object, the linear velocity will be lower, and the colliding object will move a bit (more) in its initial direction compared to a central hit.
    - If you apply a fixed force over a fixed time, the linear velocity is the same.

    Forces are not a good concept for collisions, however - they are hard to estimate and depend on details of the collision process. Momentum transfer are easier to handle.
     
  6. Jan 30, 2013 #5
    Thanks for the replies guys. I don't have any collisions, its just forces applied to the fuselage. So you say that I can calculate the force that the wing pushes with, and use that same force in both the equations to work out the linear velocity of the plane and the angular velocity? It doesn't seem to be extremely accurate though.

    Can I paste the code snippet here so you can see what I'm doing?
     
  7. Jan 30, 2013 #6

    mfb

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    Ok, the topic is a bit misleading then.
    Conservation laws are exact.
    I'm not sure if I can find time for that, but maybe others can help.
     
  8. Jan 31, 2013 #7
    Ok, thank you very much. Sorry about the topic, I thought I could figure it out if I knew the answer to the first question.

    Wing.Position is a floating point value that shows how far forward or back the wing is of the CG

    SweepMag is the magnitude of the instantaneous velocity of the wing calculated from its angular velocity.

    double SweepMag = AngularVelocity*Wing.Position;

    vector2df SweepVel = vector2df(0,1)*SweepMag;

    // I create the SweepVelocity vector and rotate it by the attitude of the aircraft

    SweepVel = SweepVel.rotateBy(Attitude,vector2df(0,0));

    vector2df ActualVel = Velocity+SweepVel;

    //The actual velocity of the air is the plane's velocity plus the wings angular instantaneous velocity

    vector2df Force = Wing.Force(Attitude,ActualVel); //function gives force vector

    vector3df ForceArm = vector3df(Wing.Position,0,0);

    TotalForce += Force; //linear force += wing force since there are multiple wings

    TotalTorque += ForceArm.crossProduct(vector3df(0,Force.getLength(),0));

    I'll explain anything in greater detail if needed. And I really appreciate the help. This forum does wonders for the world.

    What seems to be happening is that when I only have a tail plane, the aircraft doesn't dive like ad arrow, but gets enough lift from the tail plane to sway left and right in its fall significantly. Thus leading me to think I apply too much force to linear movement when it should almost only be angular.
     
  9. Feb 1, 2013 #8

    mfb

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    I don't see an error in the formulas, but they might be too simple. For the force on a wing, there might be more parameters than just the 2d-motion of its center of gravity (which can be different from the center of drag anyway) and attitude.
     
  10. Feb 1, 2013 #9
    Thanks, I found an error in my code at some other place which corrected itself by causing extreme values. This made the torque dampened out compared to the linear force. It all works now. I realize it's not perfectly accurate, but it's good enough to be fun.
     
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