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The Aeronautical Journal is a peer-reviewed journal published by Cambridge University Press, covering Diverse Scientific and Economic Studies, Human auditory perception and evaluation, Fluid Dynamics and Turbulent Flows.
| Publisher | Cambridge University Press |
|---|---|
| Reference style | Numbered Numbered — [1], [2] in the text [1] A. Smith, B. Jones, and C. Lee, A representative article title, The Aeronautical Journal 12 (2023) 45–58.
Formats any DOI in the closest standard style — The Aeronautical Journal has no published style definition, so this is an approximation. No sign-up. |
| Publishes research in | Diverse Scientific and Economic Studies Human auditory perception and evaluation Fluid Dynamics and Turbulent Flows Computational Fluid Dynamics and Aerodynamics Educational Robotics and Engineering |
| ISSN | 0001-9240 |
| Citation impact (2-yr) | 1.8 |
| h-index | 68 |
| i10-index | 1,067 |
| Total citations | 39,721 |
| Top institutions publishing here | Cranfield University |
| Journal website | www.cambridge.org |
| You get | A submission-ready PDF and the editable LaTeX source — ready to submit. |
Citations each year’s papers have accumulated so far — the most recent years are still building up.
The problem of impact damage in laminated composite structures, and the consequent reduction in residual strength, has been a topic of continual research for over two decades. The number of journal papers on the subject now runs into four figures and most have been conscientiously reviewed by Abrate(1991, 1994, 1998). This review is not intended…
Abstract A review of morphing concepts with a strong focus on morphing skins is presented. Morphing technology on aircraft has found increased interest over the last decade because it is likely to enhance performance and efficiency over a wider range of flight conditions. For example, a radical change in configuration, i.e. wing geometry in flight…
The analytical construction of displacement functions for plate elements subject to bending was discussed at some length in ref. 1. Attention was thereby drawn to both triangular and quadrilateral elements available in the ASKA system, which satisfy either all kinematic compatibility conditions or are deficient in the continuity of the gradient normal to the edge.…
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Even with today’s computers, a wind tunnel is an essential tool in engineering, both for model tests and basic research. Since the 1930s, when the strong effect of free-stream turbulence on shear layers became apparent, emphasis has been laid on wind tunnels with low levels of turbulence and unsteadiness. Consequently most high performance wind tunnels…
