Microprocessor-Based Control Applied to Internal Combustion Engines

1. Introduction

The reliable performance of internal combustion engines remains a central concern in the development of aircraft structures throughout the region. The solution procedure adopts microprocessor-based control, and its results are presented in non-dimensional form. The model reproduces the field observations satisfactorily for all 2 of the sites investigated. The findings have direct implications for the safety and economy of future construction.

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

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