By Sergey Nazarenko

**Fluid Dynamics through Examples and Solutions** presents a considerable set of instance difficulties and exact version ideas overlaying a variety of phenomena and results in fluids. The ebook is perfect as a complement or examination evaluate for undergraduate and graduate classes in fluid dynamics, continuum mechanics, turbulence, ocean and atmospheric sciences, and similar parts. it's also appropriate as a chief textual content for fluid dynamics classes with an emphasis on studying by way of instance and as a self-study source for training scientists who have to examine the fundamentals of fluid dynamics.

The writer covers a number of sub-areas of fluid dynamics, sorts of flows, and functions. He additionally comprises supplementary theoretical fabric whilst worthy. every one bankruptcy offers the historical past, a longer record of references for extra studying, various difficulties, and an entire set of version solutions.

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**Extra info for Fluid dynamics via examples and solutions**

**Sample text**

The incompressibility condition in terms of the velocity field is ∇·u = 0. The vorticity field satisfies the same equation, ∇ · ω = 0, by virtue of its definition ω = ∇ × u: because the divergence of any curl is zero, ∇ · (∇ × u) = 0. 2. Using the definition of the material time derivative, the conservation of the field s along the trajectories of fluid particles is Dt s ≡ ∂t s + u · ∇s = 0. 30) 3. 27), we have the vorticity evolution equation: ∂t ω = ∇ × (u × ω) + (∇ρ × ∇p)/ρ2 . 31) 4. If the passive scalar s(x, t) depends on x and t only via p and ρ, s = s(p, ρ) ∇s · (∇ρ × ∇p) = [(∂ρ s)∇ρ + (∂p s)∇p] · (∇ρ × ∇p) = 0 for both barotropic and baroclinic fluids.

Velocity of the emerging jet is independent of the distance from its centre. 1: Tap water. 1. Consider the part of the jet which is of sufficient distance away from the point of impact with the solid surface, where we can assume that velocity remains independent of the distance from the jet’s centre. Find the jet velocity u and its diameter d as function of the distance z from the tap. 2. Now consider the impact part of the flow in the vicinity of the solid plane. 1. 2. A valve is located at the farthest point from the barrel end of the pipe with maximal opening equal to the full cross-section of the pipe.

On the other hand, if there is separation (bluff body shape), then the pressure behind the body will not recover to the levels of the upstream flow as would be prescribed by Bernoulli’s theorem. This disbalance of the upstream and the downstream pressures would cause a finite drag. 12 1. By Bernoulli’s theorem, p1 − p0 = ρ 2 u . 64) 2. e. (p1 − p0 )sm . e. ρu2 sj : (p1 − p0 )sm = ρu2 sj . 5. 13 1. The pressure at the water surface and the one at the jet are both equal to the atmospheric pressure.