Modeling of the Transient Response for Compressible Air Cushion Vehicles (ACV)

Article Preview

Abstract:

A model for compressible Air Cushion Vehicles (ACV) is presented. In this model the compressible Bernoulli's equation and the Newton's second law of motion are used to predict the dynamic behavior of the heave response of the ACV in both time and frequency domains. The mass flow rate inside the air cushion of this model is assumed to be constant. The self excited response and the cushion pressure of the ACV is calculated to understand the behavior of the system in order to assist in the design stage of such systems. It is shown in this study that the mass flow rate and the length of the vehicle's skirt are the most significant parameters which control the steady state behavior of the self excited oscillations of the ACV. An equation to predict the transient time of the oscillatory response or the settling time in terms of the system parameters of the ACV is developed. Based on the developed equations, the optimum parameters of the ACV that lead to minimum settling time are obtained.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

560-567

Citation:

Online since:

January 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] J. R. Amyot: Hovercraft Technology Economics and Applications, Elsevier Studies in Mechanical Engineering, Vol. 11, Elsevier Inc., (1989).

Google Scholar

[2] T. C. Jung: Design of Air Cushion Vehicles Using Artificial Intelligence: Expert System and Genetic Algorithm, Masters Theses, Ryerson University, Toronto, (2002).

DOI: 10.32920/ryerson.14662224

Google Scholar

[3] J. Chung and T. C. Jung: Optimization of an air cushion vehicle bag and finger skirt using genetic algorithms, Aerospace Science and Technology, no. 8, pp.219-229, (2004).

DOI: 10.1016/j.ast.2003.11.002

Google Scholar

[4] J. Zhou, J. Guo, W. Tang, , and S. Zhang: Nonlinear FEM simulation of Air Cushion Vehicle (ACV) skirt joint under tension loading, Technical Paper, American Society of Naval Engineers, (2009).

DOI: 10.1111/j.1559-3584.2009.00192.x

Google Scholar

[5] Lavis, D. R. and B. G. Forstell: Air Cushion Vehicle (ACV) development in the US, FAST2005. St. Petersburg, Russia, (2005).

Google Scholar

[6] T. Ma and P. A. Sullivan: Linear analysis of heave dynamics of a bag and finger air cushion vehicle skirt, AIAA 8th Advanced Marine System Conference, (1986).

DOI: 10.2514/6.1986-2361

Google Scholar

[7] M. J. Hinchey and P. A. Sullivan: A theoretical study of limit cycle oscillations of plenum air cushion, Journal of sound and vibration, no. 79(1), pp.61-77, (1981).

DOI: 10.1016/0022-460x(81)90329-1

Google Scholar

[8] P. A. Sullivan, J. E. Byrne and M. J. Hinchey: Non-linear oscillations of a simple flexible skirt air cushion, Journal of sound and vibration, no. 102(2), pp.269-283, (1985).

DOI: 10.1016/s0022-460x(85)80059-6

Google Scholar

[9] Doctors, L. J., The forces on air cushion vehicle executing an unsteady motion, Proceedings of the Ninth Symposium on Naval Hydrodynamics, Paris, France, (1972).

Google Scholar

[10] A. H. Nikseresht, M. M. Alishahi and H. Emdad: Complete flow field computation around an ACV (air-cushion vehicle) using 3D VOF with lagrangian propagation in computational domain, Computer and Structures, no. 86, pp.627-641, (2008).

DOI: 10.1016/j.compstruc.2007.08.006

Google Scholar

[11] W. Milewski, B. Connell and B. Petersen: Initial Validation of the ACVSIM Model for dynamics of Air Cushion Vehicles, Proceedings of the 27th Symposium on Naval Hydrodynamics, Seoul, Korea, (2008).

Google Scholar

[12] T. D. Burton: Introduction to Dynamics Systems Analysis, McGraw-Hill, Inc., New York, (1994).

Google Scholar

[13] F. M. White: Viscous Fluid Flow, McGraw-Hill, Inc., 2nd Edition, New York, (1991).

Google Scholar