13.021 – Marine Hydrodynamics, Fall 2004 Lecture 21 c 2004 MIT - Department of Ocean Engineering, All rights reserved. Copyright ° 13.021 - Marine Hydrodynamics Lecture 21 Wave Forces on a Body UP U = ωA Ul ωAl R= = ν ν UT AωT A Kc = = = 2π l l l A F CF = = f λ , ρgAl2 |{z} Wave steepness l h , R, , roughness, . . . λ λ |{z} Diffraction parameter 1 A h " UT " Kc A T " 2 A " Type of Forces Viscous forces,... (form drag, viscous drag) : f R , K c ,1.roughness f (R, Kc , roughness, . . .). Form drag (C primarily flow separation - normal stresses. D ). Associated ag form (a) associated primarily with flowwith separation wake Particle vel. drag #$ (b) Friction drag (CF ). F~ ∼ RR τω dS b.l. body S τω b.l. U forces arising from potential flow wave theory ' 2 $ p forces gy 2 force, diffraction % (Froude-Krylov " 2. Inertial force, radiation forc): forces arising from potential t & # flow wave theory. 1 If linear theory Small amplitude waves D+ ZZ ∂φ ~ Radiated F = wave potential pn̂dS where p = −ρ R ∂t + gy + body Diffracted wave potential ave al p ' % % % & (wetted surface) I t (a ) D t (b) 1 |∇φ|2 2 | {z } =0 if linear theory, small ampitude waves R t (c) $ " gy ... " " # 2 In general: φ= φI |{z} + (a) Incident wave potential ∂φI ∂t + (b.1) Diffracted wave potential p = − ρ φD |{z} ∂φD ∂t + (a) φR |{z} (b.2) Radiated wave potential + (b.1) ∂φR ∂t + gy + . . . (b.2) (a) Incident wave potential: Froude-Krylov Force approximation, when l << λ, the incident wave field is not significantly modified by the presence of the body, therefore ignore φD and φR : φ ≈ φI µ Z Z F~F K = body −ρ | ¶ ∂φI + gy n̂dS ⇐ can calculate knowing (incident) wave kinematics (and body geometry) ∂t {z } pI surface Further mathematical approximationis valid if the body is really small. After applying the divergence theorem, the above integral can be replaced by: Z Z Z F~F K = − ∇pI d∀ ≈ −∇pI | at body center body volume ∀ |{z} body volume (b) Diffraction and Radiation Forces - hydrodynamic coefficients: added mass, wave damping and wave excitation . . . (b.1) Diffraction or scattering force: when l not << λ, wave field near body will be affected even if body is stationary, so that no-flux B.C. is satisfied. 3 (b.1) Diffraction or scattering force: when ! not << ", wave field near body will be affected even if body is stationary. φI φI Stationary body φD φD φD (b.1) Diffraction or scattering force: when ! not << ", wave field near body will be ∂ (φ I + φ D ) ∂n ∂φ D I ∂φ I =− or ← givenStationary body ∂n ∂n ∂φ ∂n φD affected even if body is stationary. = 0 = I D D ! FD !! body ' %% & $ "ndS t "# D D D 0 n D or µ Z Z n D I n ¶ I n given ∂φD ! ~D ='% D $"ndS F −ρ n̂dS F D added mass " damping % and ∂t coefficient: t # & body (b.2) Radiation Force !! body even in the absence of an incident wave, body in motion creates waves and hence wave forces, and experiences also inertial forces. (b.2) Radiation Force added mass and damping (b.2) Radiation Force - added mass and damping coefficient: even incoefficient: the absence of an incident in the an incident wave, in motion creates waves and hence wave wave, body in motion creates even waves andabsence henceofwave forces, andbody experiences also inertial forces. forces, and experiences also inertial forces. ! φR φR φR ! U R n ! U n φR ! U !! ! ∂φ R = U ⋅ n ∂n ! ' $ % "'% !! & #& ' ' Added mass Added mass µ Z Z F~R = −ρ ∂φR ∂t n̂dS = − mij U̇j − dij Uj |{z} |{z} added wave mass radiation damping 4 Wave radiation damping Wave radiation damping ¶ body $ " # Important parameters (1)Kc = UT l = 2π Al (2)diffraction parameter l λ interrelated since maximum wave steepness: ¡ A ¢ ¡ l ¢ ≤ 0.07 l λ A λ ≤ 0.07 • If Kc ≤ 1: no appreciable flow separation, viscous effect confined to b.l. (hence small), solve problem via potential theory. In addition, depending on the value of the ratio λl : – If λl << 1, ignore diffraction , wave effects in radiation problem (i.e., dij ≈ 0, mij ≈ mij infinite fluid added mass). F-K approximation might be used, calculate F~F K . – If l λ >> 1/5, must consider wave diffraction, radiation ( Al ≤ 0.07 l/λ ≤ 0.035). • If Kc >> 1: separation important, viscous forces can not be neglected. Further on if: l 0.07 l ≤ so << 1 ignore diffraction and F-K approximation might be used λ A/l λ 1 F = ρl2 U (t) |U (t)|CD (R) |{z} 2 relative velocity • Intermediate Kc - both viscous and inertial effects important, use Morrison’s formula. 1 F = ρl2 U (t)|U (t)|CD (R) + ρl3 U̇ Cm (R, Kc ) 2 5 Summary: I Limiting case: wave breaking occurs II III I. Use: CD and F − K approximation. II. Use: CF and F − K approximation. III. CD is not important and F − K approximation. is not valid. 6