Model Flow Over Bombs: Rotation & Drag Coefficients

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The discussion focuses on modeling the coefficient of drag on bombs using computational fluid dynamics (CFD) to analyze flow at various angles of attack. It raises questions about whether bombs with fins rotate during free fall and how this affects drag and stability. The fins serve to stabilize the bomb's flight path, similar to arrow fletching, minimizing drag and maximizing distance and velocity. Some bombs are designed to spin for stability, while others are not, depending on their intended purpose. The conversation also touches on the use of grid fins in missiles, which increase aerodynamic drag, and the applicability of these principles to air-to-air missiles like the AIM-9 Sidewinder.
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I'm working on a project that will find the coefficient of drag on bombs with various added drag features by modeling flow over the bomb at various angles of attack using CFD.

The problem is that I'm not sure if bombs with fins rotate while they are falling due to gravity, and if so, how I can relate the velocity of the flow to the rotation rate of the bomb.

Since the fins on a bomb are flat and not curved like an impeller, do they simply keep the bomb flying on a predictable path?
 
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Same purpose as an the feathers or fins of an arrow. They keep the nose pointing in direction of travel and prevent the arrow ( bomb ) from tumbling head over heal. In this way drag is minimized along the streamlined surface of the projectile, travel distance ( especially for the arrow ) and velocity would be maximized upon reaching the target. Thus time from release to impact would be minimized which could be a desirable feature as could velocity upon impact.

A weather vane works upon the same principle.
 
Excellent. Thank you.
 
Some bombs are meant to spin as they fall towards their target. Others not; it all depends on the bomb and its purpose. Here are some examples:

Fixed fins, stability only: Paveway IV ( GBU-12 added GPS ) and the GBU-54
Read more: http://www.defencetalk.com/forums/air-force-aviation/bomb-aerodynamics-12499/#ixzz30VtqO1Nu

Fins that cause the bomb to spin:
https://share.sandia.gov/news/resources/news_releases/wind_tunnel/#.U2LllGdOVgU

Grid fins (or lattice fins) are a type of flight control surface used on missiles and bombs in place of more conventional control surfaces, such as planar fins. These fins increase the aerodynamic drag.
http://en.wikipedia.org/wiki/Grid_fin

Hundreds of images of various types of bomb fins:
https://www.google.com/search?q=bom...6JseMyASFhoCYAw&ved=0CGUQsAQ&biw=1093&bih=528

A technical paper on the subject:
JOURNAL OF THEORETICAL
AND APPLIED MECHANICS
48, 1, pp. 27-44, Warsaw 2010
MODEL OF GASODYNAMIC CONTROL SYSTEM FOR
GUIDED BOMBS
http://yadda.icm.edu.pl/yadda/eleme...c/httpwww_ptmts_org_plglebocki-zug-2010-1.pdf
 
gm3 said:
I'm working on a project that will find the coefficient of drag on bombs with various added drag features by modeling flow over the bomb at various angles of attack using CFD.

The problem is that I'm not sure if bombs with fins rotate while they are falling due to gravity, and if so, how I can relate the velocity of the flow to the rotation rate of the bomb.

Since the fins on a bomb are flat and not curved like an impeller, do they simply keep the bomb flying on a predictable path?

gm3 said:
Excellent. Thank you.

So after reading the great responses and links, can you summarize when a ballistic bomb design would be better served with rotation versus not?

And can you extrapolate to air-to-air missles, and why some may use rotation? Which ones do?
 
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