A Nonlinear Theory for a Hovercraft Moving over Regular Waves

Author:

Reynolds A. J.1

Affiliation:

1. Reader in Mechanical Engineering, Brunel University, Uxbridge, Middlesex. Member of the Institution

Abstract

The equations governing the heaving and pitching of a hovercraft supported on two interconnected plenum compartments are integrated numerically to find the response as the craft passes over sinusoidal waves whose crests are normal to the direction of motion. When the flexible skirt around the plenum chambers comes into contact with the wave profile, it is assumed to collapse against the unyielding surface of the water. The scheme of integration is explained, and predictions of accelerations experienced on the craft are compared with those from a linearized theory developed earlier. For the range of wave heights considered, the accelerations indicated by the nonlinear theory are normally higher than those of the linear theory; save near pitching resonance, the two predictions differ by less than fifty per cent. For small wave heights, the ultimate response retains significant elements linked to the natural frequencies of pitch and heave.

Publisher

SAGE Publications

Subject

General Engineering

Cited by 6 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. Analysis of Wave Load Characteristics of Hovercraft Based on Model Test;Journal of Marine Science and Engineering;2024-09-03

2. Hybrid analytic-FEM approach for dynamic response analysis of air-cushion vehicle skirts;Marine Structures;2021-09

3. Nonlinear heave dynamics of an air cushion vehicle bag and finger skirt;Flight Simulation Technologies Conference;1996-07-29

4. Pitch-heave dynamics of a segmented skirt cushion;Advanced Marine Vehicles Conference;1989-06-05

5. Non-linear oscillations of a simple flexible skirt air cushion;Journal of Sound and Vibration;1985-09

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