Hostname: page-component-cd9895bd7-gxg78 Total loading time: 0 Render date: 2024-12-28T20:21:51.316Z Has data issue: false hasContentIssue false

A Technical Note on the appropriate CFD boundary conditions for the prediction of ground effect aerodynamics

Published online by Cambridge University Press:  04 July 2016

T. J. Barber
Affiliation:
Mechanical and Manufacturing EngineeringUniversity of New South WalesSydney, New South Wales, Australia
E. Leonardi
Affiliation:
Mechanical and Manufacturing EngineeringUniversity of New South WalesSydney, New South Wales, Australia
R. D. Archer
Affiliation:
Mechanical and Manufacturing EngineeringUniversity of New South WalesSydney, New South Wales, Australia

Extract

The accurate prediction of ground effect aerodynamics is an important aspect of wing-in-ground effect vehicle (WIG) design. Computational fluid dynamics (CFD) solutions are useful alternatives to expensive (especially in the case of ground effect) wind-tunnel testing. However, the incorporation of the rigid surface effects often leads to confusion due to such a model being in a vehicle fixed reference frame (air moving, vehicle fixed) rather than the real-life situation of a ground fixed reference frame (air fixed, vehicle moving).

Type
Technical Note
Copyright
Copyright © Royal Aeronautical Society 1999 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Hsiun, C. and Chen, C. Aerodynamic characteristics of a two-dimensional airfoil with ground effect, J Aircr, 1996, 33, (2), pp 386392.Google Scholar
2. Wieselsberger, C. Wing resistance near the ground, NACA TM 77, 1922.Google Scholar
3. Steinbach, D. Comment on ‘aerodynamic characteristics of a two-dimensional airfoil with ground effect,’; J Aircr, 1997, 34, (3), pp 455456.Google Scholar
4. Barber, T., Leonardi, E. and Archer, D. A simple and effective zonal procedure for lifting surfaces, submitted to Engineering Analysis with Boundary Elements, 1999.Google Scholar
5. Kuhmstedt, T. Aerodynamic design procedure and results of the development of commercial WIG craft. Workshop Proceedings of Ekranoplans and Very Fast Craft, University of New South Wales, 5-6 December 1996, pp 20-37.Google Scholar
6. Rozhdestvensky, K. Nonlinear aerodynamics of ekranoplan in strong ground effect, Third International Conference on Fast Sea Transportation (FAST95), 23-27 September 1995, Lubeck-Travemunde, Germany, 1995, pp 621-630.Google Scholar