Question 1.3.4: Modeling Fluid Drag The drag force on an object moving throu...
Modeling Fluid Drag
The drag force on an object moving through a liquid or a gas is a function of the velocity. A commonly used model of the drag force D on an object is
D=\frac{1}{2}\rho AC_{D}v^2 \quad (1)
where 𝜌 is the mass density of the fluid, A is the object’s cross-sectional area normal to the relative flow, v is the object’s velocity relative to the fluid, and C_D is the drag coefficient, which is usually determined from wind-tunnel or water-channel tests on models. Curve A in Figure 1.3.6 is a plot of this equation for an Aerobee rocket 1.25 ft in diameter, with C_D = 0.4, moving through the lower atmosphere where 𝜌 = 0.0023 slug/ft³, for which equation (1) becomes
D=0.00056v^2 \quad (2)
a. Obtain a linear approximation to this drag function valid near v = 600 ft/sec.
b. Obtain a linear approximation that gives a conservative (high) estimate of the drag force as a function of the velocity over the range 0 ≤ v ≤ 1000 ft/sec.
Our explanations are based on the best information we have, but they may not always be right or fit every situation.
Learn more on how we answer questions.