Physics question? | FerrariChat

Physics question?

Discussion in 'Other Off Topic Forum' started by DrStranglove, Feb 17, 2007.

This site may earn a commission from merchant affiliate links, including eBay, Amazon, Skimlinks, and others.

  1. DrStranglove

    DrStranglove FChat Assassin Owner Rossa Subscribed

    Joined:
    Oct 31, 2003
    Messages:
    31,646
    Location:
    Google Maps
    Full Name:
    DrS
    My Col put this problem on the board:

    X = 1/2 p v2 S Cl

    p was something I thought he called "roe"
    s= area and Cl is coefficient.

    Any ideas what he was talking about?
     
  2. Mike328

    Mike328 F1 Rookie

    Joined:
    Oct 19, 2002
    Messages:
    2,655
    Location:
    Boulder, CO
    Full Name:
    Mike

    That is the calculation of drag (at high velocities). So a particle moving at high velocity through a "fluid" (e.g., air) is going to experience a force against its direction of motion. This equation tells you what that force is.


    See Wikipedia on Drag:
    http://en.wikipedia.org/wiki/Drag_(physics)

    p is lowercase greek letter "ro"
    v is velocity of the particle


    So this equation would come into play when figuring out the path of a bullet or some other particle in the air (also applies to flight dynamics) because you have to factor in the force of the drag acting on that bullet/particle (i.e., in reality, things don't happen in a "vacuum!" [at least not in the Earth's atmosphere!]).

    Edit: This also relates to the concept of "terminal velocity," since at some point, the drag force (acting UP against a falling object) will grow so great as to cancel out the force of gravity acting on that same object.
     
  3. ylshih

    ylshih Shogun Assassin Honorary Owner

    Joined:
    Mar 21, 2004
    Messages:
    20,538
    Location:
    Northern CA
    Full Name:
    Yin
    It looks like the equation for lift of an airfoil.

    Lift Force = 1/2 * rho * V^2 * A * Cl

    rho = air density
    V = velocity (V^2 means velocity squared)
    A = surface area of the airfoil
    Cl = coefficient of lift (value has to be determined for a specific airfoil shape)

    Edit: it's actually the same equation as for drag, but since he gave the coefficient as Cl, not Cd, then it's more likely for lift :).
     
  4. LMPDesigner

    LMPDesigner F1 Rookie Silver Subscribed

    Joined:
    Nov 5, 2003
    Messages:
    3,209
    Location:
    Atlanta Georgia
    Its an equation for the lift of a wing, car, object, etc. Drag equation is same but substitute Cd for Cl.
     
  5. LZeitgeist

    LZeitgeist Karting

    Joined:
    Mar 23, 2005
    Messages:
    190
    Location:
    Raleigh, NC - USA
    Full Name:
    Patrick
    Actually, 'rho'.
     
  6. Mike328

    Mike328 F1 Rookie

    Joined:
    Oct 19, 2002
    Messages:
    2,655
    Location:
    Boulder, CO
    Full Name:
    Mike
    Correct, I meant to correct the "roe" and blew it myself!
     
  7. RacerX_GTO

    RacerX_GTO F1 World Champ Silver Subscribed

    Joined:
    Nov 2, 2003
    Messages:
    14,826
    Location:
    Oregon
    Full Name:
    Gabe V.
    Math problems? Call 1-800-{(10x)(13i)2}-{sin(xy)/2.362x}.
     

Share This Page