This works has been made within a project with the CNES (French National Center for Space Studies, during my studies in aeronautic engineer high school), within the project for the study of the sizing of the lauching pad of Ariane 5 project sattelite launcher.

I have made a lot of research to find if this theroem was known or not ?

I had never never found a reference ? May you help me please.

Before the theorem statement, just few recall :

1/ The aerodynamic drag is given (within special domain) traditionaly by : 1/2 Cx ro S v^2

    (ro being the air density, v the velocity (relative to air flow), and Cx the so called penetration coefficient)

    The term of interest in the problem is the S, which is called the "master couple, french traduction of the term used in french" which represents the projection surface of the body on a plan perpendicular to it's trajectory vector.

2/ The theorem I have demonstrated is the following statement :

   " The average master couple for any convex body over all orientations (then integrated over unit sphere, for projection axis) is equal to the "Exterior Surface of the body" divided by 4. "

[this is an evidence for the particular case of the sphere : 4 pi R2 / 4 = pi R2 projected surface equal everywhere]

I know that at the epoch, these formula was used by persons as an heurisic ?

3/ But my definitive questions are :

Is this theorem relevant or not ?

Is it an obvious corollary of convex mathematics ?

(which is from my point of view certainly the case) ?

PS = I have also demonstrated the exact formula for only one particular non convex body (in fact a surface, but this is just a question of factor 2) which is an angular part of a section of a cylinder). This is not really difficult but hardly analysis computational !

and an approximation formula for non convex body (but I do not realy know the quality)

and other few relative theorems (like the result for the union of two convex body creating another convex body)

Thx in advance for any kind of answer ?

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