Difference between revisions of "Long Wavelength Approximations"
Line 5: | Line 5: | ||
}} | }} | ||
− | = Introduction = | + | == Introduction == |
Very frequently the length of ambient waves <math> \lambda \,</math> is large compared to the dimension of floating bodies. | Very frequently the length of ambient waves <math> \lambda \,</math> is large compared to the dimension of floating bodies. | ||
Line 11: | Line 11: | ||
− | = GI Taylor's formula = | + | == GI Taylor's formula == |
Consider a flow field given by | Consider a flow field given by | ||
Line 31: | Line 31: | ||
<center><math> \ A_{11}: \ \mbox{Surge added mass} \,</math></center> | <center><math> \ A_{11}: \ \mbox{Surge added mass} \,</math></center> | ||
− | == Derivation using Euler's equations == | + | === Derivation using Euler's equations === |
An alternative form of GI Taylor's formula for a fixed body follows from Euler's equations: | An alternative form of GI Taylor's formula for a fixed body follows from Euler's equations: | ||
Line 47: | Line 47: | ||
Often, when the ambient velocity <math> U\,</math> is arising from plane progressive waves, <math> \left| U \frac{\partial U}{\partial X} \right| = 0(A^2) \,</math> and is omitted. Note that <math> U\,</math> does not include disturbance effects due to the body. | Often, when the ambient velocity <math> U\,</math> is arising from plane progressive waves, <math> \left| U \frac{\partial U}{\partial X} \right| = 0(A^2) \,</math> and is omitted. Note that <math> U\,</math> does not include disturbance effects due to the body. | ||
− | = Applications of GI Taylor's formula in wave-body interactions = | + | == Applications of GI Taylor's formula in wave-body interactions == |
− | == Archimedean hydrostatics == | + | === Archimedean hydrostatics === |
<center><math> P=-\rho g Z, \quad \frac{\partial P}{\partial Z} = - \rho g \,</math></center> | <center><math> P=-\rho g Z, \quad \frac{\partial P}{\partial Z} = - \rho g \,</math></center> | ||
Line 60: | Line 60: | ||
is no flow. This offers an intuitive meaning to the term that includes the body displacement. | is no flow. This offers an intuitive meaning to the term that includes the body displacement. | ||
− | == Regular waves over a circle fixed under the free surface == | + | === Regular waves over a circle fixed under the free surface === |
<center><math> \Phi_I = \mathrm{Re} \left\{ \frac{i g A}{\omega} e^{KZ-iKX+i\omega t} \right\}, \quad K=\frac{\omega^2}{g} \, </math></center> | <center><math> \Phi_I = \mathrm{Re} \left\{ \frac{i g A}{\omega} e^{KZ-iKX+i\omega t} \right\}, \quad K=\frac{\omega^2}{g} \, </math></center> | ||
Line 82: | Line 82: | ||
We can derive the vertical force along very similar lines. It is simply <math>90^\circ\,</math> out of phase relative to <math>F_X\,</math> with the same modulus. | We can derive the vertical force along very similar lines. It is simply <math>90^\circ\,</math> out of phase relative to <math>F_X\,</math> with the same modulus. | ||
− | == Horizontal force on a fixed circular cylinder of draft <math>T\,</math> == | + | === Horizontal force on a fixed circular cylinder of draft <math>T\,</math> === |
This case arises frequently in wave interactions with floating offshore platforms. | This case arises frequently in wave interactions with floating offshore platforms. | ||
Line 115: | Line 115: | ||
\,</math> | \,</math> | ||
− | == Horizontal force on multiple vertical cylinders in any arrangement | + | === Horizontal force on multiple vertical cylinders in any arrangement === |
The proof is essentially based on a phasing argument. Relative to the reference frame: | The proof is essentially based on a phasing argument. Relative to the reference frame: | ||
Line 142: | Line 142: | ||
* The above technique may be easily extended to estimate the Sway force and Yaw moment on n-cylinders with little extra effort. | * The above technique may be easily extended to estimate the Sway force and Yaw moment on n-cylinders with little extra effort. | ||
− | == Surge exciting force on a 2D section == | + | === Surge exciting force on a 2D section === |
<center><math> \Phi_I = \mathfrak{Re} \left\{ \frac{ i g A}{\omega} e^{KZ-iKX+i\omega t} \right\} \,</math></center> | <center><math> \Phi_I = \mathfrak{Re} \left\{ \frac{ i g A}{\omega} e^{KZ-iKX+i\omega t} \right\} \,</math></center> | ||
Line 160: | Line 160: | ||
So in long waves, the surge exciting force is equally divided between the Froude-Krylov and the diffraction components. This is not the case for Heave! | So in long waves, the surge exciting force is equally divided between the Froude-Krylov and the diffraction components. This is not the case for Heave! | ||
− | == Heave exciting force on a surface piercing section == | + | === Heave exciting force on a surface piercing section === |
In long waves, the leading order effect in the exciting force is the hydrostatic contribution: | In long waves, the leading order effect in the exciting force is the hydrostatic contribution: |
Revision as of 11:31, 10 April 2009
Wave and Wave Body Interactions | |
---|---|
Current Chapter | Long Wavelength Approximations |
Next Chapter | Wave Scattering By A Vertical Circular Cylinder |
Previous Chapter | Added-Mass, Damping Coefficients And Exciting Forces |
Introduction
Very frequently the length of ambient waves [math]\displaystyle{ \lambda \, }[/math] is large compared to the dimension of floating bodies. For example the length of a wave with period [math]\displaystyle{ T=10 \ \mbox{sec}\, }[/math] is [math]\displaystyle{ \lambda \simeq T^2 + \frac{T^2}{2} \simeq 150\mbox{m} \, }[/math]. The beam of a ship with length [math]\displaystyle{ L=100\mbox{m}\, }[/math] can be [math]\displaystyle{ 20\mbox{m}\, }[/math] as is the case for the diameter of the leg of an offshore platform.
GI Taylor's formula
Consider a flow field given by
[math]\displaystyle{ U(X,t):\ \mbox{Velocity of ambient unidirectional flow} \, }[/math]
[math]\displaystyle{ P(X,t):\ \mbox{Pressure corresponding to} \ U(X,t) \, }[/math]
In the absence of viscous effects and to leading order for [math]\displaystyle{ \lambda \gg B \, }[/math]:
where
Derivation using Euler's equations
An alternative form of GI Taylor's formula for a fixed body follows from Euler's equations:
Thus:
If the body is also translating in the X-direction with displacement [math]\displaystyle{ X_1(t)\, }[/math] then the total force becomes
Often, when the ambient velocity [math]\displaystyle{ U\, }[/math] is arising from plane progressive waves, [math]\displaystyle{ \left| U \frac{\partial U}{\partial X} \right| = 0(A^2) \, }[/math] and is omitted. Note that [math]\displaystyle{ U\, }[/math] does not include disturbance effects due to the body.
Applications of GI Taylor's formula in wave-body interactions
Archimedean hydrostatics
So Archimedes' formula is a special case of GI Taylor when there is no flow. This offers an intuitive meaning to the term that includes the body displacement.
Regular waves over a circle fixed under the free surface
So the horizontal force on the circle is:
Thus:
We can derive the vertical force along very similar lines. It is simply [math]\displaystyle{ 90^\circ\, }[/math] out of phase relative to [math]\displaystyle{ F_X\, }[/math] with the same modulus.
Horizontal force on a fixed circular cylinder of draft [math]\displaystyle{ T\, }[/math]
This case arises frequently in wave interactions with floating offshore platforms.
Here we will evaluate [math]\displaystyle{ \frac{\partial u}{\partial t} \, }[/math] on the axis of the platform and use a strip wise integration to evaluate the total hydrodynamic force.
The differential horizontal force over a strip [math]\displaystyle{ d Z \, }[/math] at a depth [math]\displaystyle{ Z \, }[/math] becomes:
The total horizontal force over a truncated cylinder of draft [math]\displaystyle{ T\, }[/math] becomes:
This is a very useful and practical result. It provides an estimate of the surge exciting force on one leg of a possibly multi-leg platform As [math]\displaystyle{ T \to \infty; \quad \frac{1-e^{-KT}}{K} \to \frac{1}{K} \, }[/math]
Horizontal force on multiple vertical cylinders in any arrangement
The proof is essentially based on a phasing argument. Relative to the reference frame:
- Express the incident wave relative to the local frames by
introducing the phase factors:
Let:
Then relative to the i-th leg:
Ignoring interactions between legs, which is a good approximation in long waves, the total exciting force on an n-cylinder platform is:
The above expression gives the complex amplitude of the force with [math]\displaystyle{ \mathbf{X}_1\, }[/math] given in the single cylinder case.
- The above technique may be easily extended to estimate the Sway force and Yaw moment on n-cylinders with little extra effort.
Surge exciting force on a 2D section
- If the body section is a circle with radius [math]\displaystyle{ a\, }[/math]:
So in long waves, the surge exciting force is equally divided between the Froude-Krylov and the diffraction components. This is not the case for Heave!
Heave exciting force on a surface piercing section
In long waves, the leading order effect in the exciting force is the hydrostatic contribution:
where [math]\displaystyle{ A_w\, }[/math] is the body water plane area in 2D or 3D. [math]\displaystyle{ A\, }[/math] is the wave amplitude. This can be shown to be the leading order contribution from the Froude-Krylov force
Using the Taylor series expansion:
It is easy to verify that: [math]\displaystyle{ \mathbf{X}_3 \to \rho g A A_w \, }[/math].
The scattering contribution is of order [math]\displaystyle{ KB\, }[/math]. For submerged bodies: [math]\displaystyle{ \mathbf{X}_3^{FK}=O(KB)\, }[/math].
This article is based on the MIT open course notes and the original article can be found here
Ocean Wave Interaction with Ships and Offshore Energy Systems