NIWC Drag on Inline String of Spheres

Spring 2021 MAE 156b Sponsored Project

University of California San Diego

Sponsors: Mark Gillcrist, and Sal Serra of Naval Information Warfare Center (NIWC)

Background:

Naval Information Warfare Center (NIWC) Pacific develops seafloor hardware that support a wide range of Navy missions. Installation of seafloor equipment is often accomplished by dropping the item overboard with a string of trailing floats as shown in Figure 1. The floats reduce the in-water weight (defined as the difference of the buoyancy and force of gravity on the system) of the deployment package, enhance stability, and position the equipment in a preferred orientation. By judiciously selecting a number of floats, a desired terminal descent speed can be achieved. If the descent rate is too fast, the equipment could be damaged on impact with the seabed. If the descent is too slow, the package could be carried by currents far from the intended touch-down site. The terminal descent velocity can be accurately estimated if the in water weight and drag of the equipment are known and the buoyancy and drag of the trailing floats are known.

This project investigates drag of the trailing floats. Said floats are close to spherical, and are treated as such. While drag on a single sphere is well established, there is little literature on the drag of several attached in line. What is known is if the floats are close enough together, the wake of the leading floats will decrease the drag induced by the following floats. This effect is expected to decrease as the separation distance increases. Eventually, at a large enough distance the leading float's wake stop effecting following float's drag. It's also assumed that drag contribution of following floats will be constant by this point.

Figure 1: Notional Deployment with String of In-line Trailing Floats

Project Goals

To determine the drag contribution of additional floats an experimental system consisting of float(s), weight(s), and depth sensors was used. Said system was dropped in water deep enough to reach and stay at terminal velocity for a substantial time period. Terminal velocity data was then used to determine the system's drag. This process was repeated for:

  • 1 Sphere / Float; To create a baseline from which drag contributions can be derived from

  • 2 Spheres / Floats at various separations; To determine drag contribution of additional spheres

  • 2-5 Spheres / Floats at 0cm separation; To further explore drag contribution of additional spheres

Experimental System

Results:

1-sphere configuration:


2-sphere configurations:

Data collected at Canyonview with a splint between the two floats proved to be the most reliable. This gives the empirical formula below for the drag coefficient where x represents the separation distance between spheres.

Cd = 0.293x0.276 + 0.723

2-5 sphere configurations with 0cm separation distance:

All configurations with three or more inline spheres were tested with 0cm separation between the spheres.

Cd = 5.631e-1.26nsin(1.468n) + 0.7864

Senior Day Presentation:

0Senior Day Pres.pptx

Senior Day Presentation Recording:

Ivy_Alex.mp4