Heave Stiffness of an Air Cushion Vehicle Bag-and-Finger Skirt

Author:

Sullivan P. A.1,Charest P. A.2,Ma T.3

Affiliation:

1. University of Toronto

2. Spar Aerospace Ltd

3. Marine Design and Research Institute of China

Abstract

The heave stiffness of a bag-and-finger flexible skirt air cushion is investigated analytically and experimentally. The investigations use a two-dimensional section of the skirt confined between end-plates and moving in heave. This simplified geometry facilitates analysis involving a minimum of empiricism. Experiments show that the airflows, including leaks between fingers and at the end-plates, can be modeled as orifice-like. The analysis assumes that the fingers can be modeled as rigid massless bodies. Three models of the bag, based on combinations of massless inelastic membranes and rigid links, are investigated. The predictions and experiments are in good agreement and show that modest geometry changes can have large effects on heave stiffness. It is suggested that these simple skirt models can provide useful insights into the dynamics.

Publisher

The Society of Naval Architects and Marine Engineers

Subject

Applied Mathematics,Mechanical Engineering,Ocean Engineering,Numerical Analysis,Civil and Structural Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical and experimental study of kelvin-helmholtz instabilities beneath air-cushion vehicle skirts;Ocean Engineering;2024-09

2. CFD analysis of a round shaped air cushion vehicle with flexible skirt segments at 90° and different air clearance height;IOP Conference Series: Materials Science and Engineering;2020-12-01

3. A FEM fluid–structure interaction algorithm for analysis of the seal dynamics of a Surface-Effect Ship;Computer Methods in Applied Mechanics and Engineering;2015-10

4. TO STUDY AND FABRICATION OF AIR CUSHION VEHICLE;International Journal of Research -GRANTHAALAYAH;2015-03-31

5. Linear Heave Dynamics of an Air-Cushion Vehicle Bag-and-Finger Skirt.;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2000

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