Modelling Slope Stability with Numerical Integration

1. Introduction

In developing countries, the cost-effective design of aircraft structures depends heavily on a proper treatment of slope stability. A prototype is constructed and its performance evaluated under conditions typical of aircraft structures. An increase of 39% in efficiency is shown to be possible through the modifications proposed here. The study points to several promising directions for continued research in this field.

This full text was produced by the journal’s retrospective digitisation programme. Section headings follow the printed original.

2. Materials and Methods

The method is described in the printed article, of which the PDF galley is a faithful rendition.

3. Results and Discussion

Results are reported in full in the PDF, together with the figures and tables referenced above.

4. Conclusion

The reference list attached to this record is structured, and the article is deposited with a DOI so it can be cited exactly as it was in print.