Aérodynamic ! #altitude#temperature#pressure

Discussion in 'Science' started by Bastien, Sep 28, 2013.

  1. Bastien

    Bastien New Member

    Joined:
    Sep 28, 2013
    Messages:
    6
    Likes Received:
    0
    Trophy Points:
    0
    I study the book of A.BOISSON called l'aerodynamic du vol de l'avion (french book). In this book, At the end of the first chapter you have to follow the demonstration of the error margin between the altitude given by the at mosphere standard and the real altitude in the real athmosphere according to the temperature.

    This is the demonstration: img045.jpg img044.jpg

    So I understand that dp/p=-gdZ/RT(0)+aZ no problem but the next line I can't understand why they use the logarithme ? Someone can explain me ?
     
  2. Herkdriver

    Herkdriver New Member

    Joined:
    Mar 6, 2007
    Messages:
    21,346
    Likes Received:
    297
    Trophy Points:
    0
    Je ne parle pas francais
    Therefore I don't understand the context of the question.

    The formulas I'm familiar with which appear to correlate with your image are the equation for static equilibrium
    dp = -rgdz

    Ideal gas law
    p= rRT

    The atmospheric temperature gradient
    dT/dz

    I'm not familiar with Laplace's equation, typically the relationship between the temperature and pressure of the atmosphere during adiabatic expansion is expressed in Poisson's equation.

    I'm of no help to you as my atmospheric studies are rusty. I wouldn't think too many people on a political oriented website would be able to answer your question either. I would try a physics forum, or more specifically atmospheric science.

    Au revoir
     
  3. Bastien

    Bastien New Member

    Joined:
    Sep 28, 2013
    Messages:
    6
    Likes Received:
    0
    Trophy Points:
    0
    Yes, I was surprise to see a topic in science so I tried. I will see the Poissnon's equation. If I succed in my resolving I will inform you quickly ! Thank to you !
     

Share This Page