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AOE 5104 Class 5 9/9/08 Online presentations for next class:
Equations of Motion 1 Homework 2 due 9/11 (w. recitations, this evenings is in Whitemore 349 at 5) Office hours tomorrow will start at 4:30-4:45pm (and I will stay late)
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Review Gradient Divergence Curl
For velocity: twice the circumferentially averaged angular velocity of a fluid particle = Vorticity Ω Magnitude and direction of the slope in the scalar field at a point For velocity: proportionate rate of change of volume of a fluid particle Gradient Divergence Curl
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Differential Forms of the Divergence
Cartesian Cylindrical Spherical
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Curl Elemental volume with surface S e n dS Perimeter Ce Area
dS=dsh radius a v avg. tangential velocity = twice the avg. angular velocity about e
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Review Gradient Divergence Curl
For velocity: twice the circumferentially averaged angular velocity of a fluid particle = Vorticity Ω Magnitude and direction of the slope in the scalar field at a point For velocity: proportionate rate of change of volume of a fluid particle Gradient Divergence Curl
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Integral Theorems and Second Order Operators
AOE 5104 Class 5 9/5/06 Assignments: Collect HW1 Homework 2, due 9/12/06 Online presentation “Equations of Motion 1”
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George Gabriel Stokes 1819-1903
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1st Order Integral Theorems
Volume R with Surface S Gradient theorem Divergence theorem Curl theorem Stokes’ theorem ndS d Open Surface S with Perimeter C ndS
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The Gradient Theorem Finite Volume R Surface S
Begin with the definition of grad: Sum over all the d in R: d We note that contributions to the RHS from internal surfaces between elements cancel, and so: nidS di+1 Recognizing that the summations are actually infinite: ni+1dS di
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Assumptions in Gradient Theorem
A pure math result, applies to all flows However, S must be chosen so that is defined throughout R S Submarine surface
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Flow over a finite wing S1 S1 S2 S = S1 + S2 R is the volume of fluid enclosed between S1 and S2 p is not defined inside the wing so the wing itself must be excluded from the integral
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1st Order Integral Theorems
Volume R with Surface S Gradient theorem Divergence theorem Curl theorem Stokes’ theorem ndS d Open Surface S with Perimeter C ndS
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Alternative Definition of the Curl
Perimeter Ce Area ds
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Stokes’ Theorem Finite Surface S With Perimeter C
Begin with the alternative definition of curl, choosing the direction e to be the outward normal to the surface n: n Sum over all the d in S: d Note that contributions to the RHS from internal boundaries between elements cancel, and so: dsi+1 di+1 Since the summations are actually infinite, and replacing with the more normal area symbol S: dsi di
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Stokes´ Theorem and Velocity
Apply Stokes´ Theorem to a velocity field Or, in terms of vorticity and circulation What about a closed surface?
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Assumptions of Stokes´ Theorem
A pure math result, applies to all flows However, C must be chosen so that A is defined over all S 2D flow over airfoil with =0 C The vorticity doesn’t imply anything about the circulation around C
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Flow over a finite wing C S Wing with circulation must trail vorticity. Always.
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Vector Operators of Vector Products
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Convective Operator = change in density in direction of V, multiplied by magnitude of V
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Second Order Operators
The Laplacian, may also be applied to a vector field. So, any vector differential equation of the form B=0 can be solved identically by writing B=. We say B is irrotational. We refer to as the scalar potential. So, any vector differential equation of the form .B=0 can be solved identically by writing B=A. We say B is solenoidal or incompressible. We refer to A as the vector potential.
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Class Exercise Make up the most complex irrotational 3D velocity field you can. ? We can generate an irrotational field by taking the gradient of any scalar field, since I got this one by randomly choosing And computing
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2nd Order Integral Theorems
Green’s theorem (1st form) Green’s theorem (2nd form) Volume R with Surface S ndS d These are both re-expressions of the divergence theorem.
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