Propulsive efficiency of a biomorphic pulsed-jet underwater vehicle

Ali Moslemi, Paul S. Krueger

Bioinspiration & Biomimetics · 2010 · 69 citations · 19 references

Concepts

TL;DR

The authors experimentally evaluated the propulsive efficiency of a biomorphic pulsed‑jet vehicle, Robosquid, by varying jet slug length‑to‑diameter ratios (2–6) and Strouhal numbers (0.2–0.6) with triangular or trapezoidal velocity programs, measuring jet impulse and energy via digital particle image velocimetry, and comparing the results to an equivalent steady jet while presenting a simple model linking efficiency to nozzle over‑pressure and vortex ring formation. Robosquid achieved Reynolds numbers of 1,300–2,700, and the study found that trapezoidal velocity programs yielded up to 20 % higher propulsive efficiency than triangular ones, with the efficiency ratio to an equivalent steady jet increasing as Strouhal number rose and slug length‑to‑diameter decreased—reaching a maximum of 1.2 for short L/D and high St(L)—demonstrating that pulsed jets can outperform steady jets and that changes in St(L) exert a proportionally larger influence on efficiency than changes in L/D.

Abstract

The effect of the velocity program and duty cycle (St(L)) on the propulsive efficiency of pulsed-jet propulsion was studied experimentally on a self-propelled, pulsed-jet underwater vehicle, dubbed Robosquid due to the similarity of essential elements of its propulsion system with squid jet propulsion. Robosquid was tested for jet slug length-to-diameter ratios (L/D) in the range 2-6 and St(L) in the range 0.2-0.6 with jet velocity programs commanded to be triangular or trapezoidal. Digital particle image velocimetry was used for measuring the impulse and energy of jet pulses to calculate the pulsed-jet propulsive efficiency and compare it with an equivalent steady jet system. Robosquid's Reynolds number (Re) based on average vehicle velocity and vehicle diameter ranged between 1300 and 2700 for the conditions tested. The results indicated better propulsive efficiency of the trapezoidal velocity program (up to 20% higher) compared to the triangular velocity program. Also, an increase in the ratio of the pulsed-jet propulsive efficiency to the equivalent steady jet propulsive efficiency (eta(P)/eta(P, ss)) was observed as St(L) increased and L/D decreased. For cases of short L/D and high St(L), eta(P)/eta(P, ss) was found to be as high as 1.2, indicating better performance of pulsed jets. This result demonstrates a case where propulsion using essential elements of a biological locomotion system can outperform the traditional mechanical system equivalent in terms of efficiency. It was also found that changes in St(L) had a proportionately larger effect on propulsive efficiency compared to changes in L/D. A simple model is presented to explain the results in terms of the contribution of over-pressure at the nozzle exit plane associated with the formation of vortex rings with each jet pulse.

References

19