TY - JOUR
T1 - Added mass energy recovery of octopus-inspired shape change
AU - Steele, S. C.
AU - Weymouth, G. D.
AU - Triantafyllou, M. S.
PY - 2017
Y1 - 2017
N2 - Dynamic shape change of the octopus mantle during fast jet escape manoeuvres results in added mass energy recovery to the energetic advantage of the octopus, giving escape thrust and speed additional to that due to jetting alone. We show through numerical simulations and experimental validation of overall wake behaviour, that the success of the energy recovery is highly dependent on shrinking speed and Reynolds number, with secondary dependence on shape considerations and shrinking amplitude. The added mass energy recovery ratio ηma, which measures momentum recovery in relation to the maximum momentum recovery possible in an ideal flow, increases with increasing the non-dimensional shrinking parameter σ∗ = ȧmax/URe0, where ȧmax is the maximum shrinking speed, U is the characteristic flow velocity and Re0 is the Reynolds number at the beginning of the shrinking motion. An estimated threshold σ∗∼10 determines whether or not enough energy is recovered to the body to produce net thrust. Since there is a region of high transition for 10 < σ∗ < 30 where the recovery performance varies widely and for σ∗ > 100 added mass energy is recovered at diminishing returns, we propose a design criterion for shrinking bodies to be in the range of 50 < σ∗ < 100, resulting in 61-82% energy recovery.
AB - Dynamic shape change of the octopus mantle during fast jet escape manoeuvres results in added mass energy recovery to the energetic advantage of the octopus, giving escape thrust and speed additional to that due to jetting alone. We show through numerical simulations and experimental validation of overall wake behaviour, that the success of the energy recovery is highly dependent on shrinking speed and Reynolds number, with secondary dependence on shape considerations and shrinking amplitude. The added mass energy recovery ratio ηma, which measures momentum recovery in relation to the maximum momentum recovery possible in an ideal flow, increases with increasing the non-dimensional shrinking parameter σ∗ = ȧmax/URe0, where ȧmax is the maximum shrinking speed, U is the characteristic flow velocity and Re0 is the Reynolds number at the beginning of the shrinking motion. An estimated threshold σ∗∼10 determines whether or not enough energy is recovered to the body to produce net thrust. Since there is a region of high transition for 10 < σ∗ < 30 where the recovery performance varies widely and for σ∗ > 100 added mass energy is recovered at diminishing returns, we propose a design criterion for shrinking bodies to be in the range of 50 < σ∗ < 100, resulting in 61-82% energy recovery.
KW - biological fluid dynamics
KW - propulsion
KW - wakes
UR - http://www.scopus.com/inward/record.url?scp=85028247984&partnerID=8YFLogxK
U2 - 10.1017/jfm.2016.701
DO - 10.1017/jfm.2016.701
M3 - Article
AN - SCOPUS:85028247984
SN - 0022-1120
VL - 810
SP - 155
EP - 174
JO - Journal of Fluid Mechanics
JF - Journal of Fluid Mechanics
ER -