lukus09
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Approximetly how much is the drag coefficient if orginally the coefficient is 0.02689. I know it depends on aircraft etc but I am only looking a rough estimate.
The discussion revolves around estimating the increase in drag coefficient due to the addition of spoilers on aircraft. Participants are exploring the impact of spoilers on aerodynamic drag, particularly in the context of modeling braking systems.
Participants have not reached a consensus on the exact increase in drag coefficient due to spoilers, and multiple viewpoints regarding the modeling approach and resources remain present.
The discussion does not clarify specific assumptions regarding the conditions under which the drag coefficient is estimated, nor does it resolve the mathematical steps involved in the modeling process.
Individuals interested in aerodynamics, aircraft design, and modeling of braking systems may find this discussion relevant.
Cyrus said:As a first order guess, spoilers are a flat plate. But, what outside sources have you consulted?