Journal of Aerospace Engineering & Technology

Increased demand for sustainable materials in the aerospace industry has stimulated the research of natural fibre reinforced polymer composites for specific use in the interior of aircraft. The present work explores the feasibility of jute/kenaf composite hybrid biocomposites for use in aircraft food tray with emphasis on fabrication of jute/kenaf hybrid composites, impact damage analysis of jute/kenaf hybrid composites and environmental issues.

Spacecraft trajectory design is fundamentally a mathematical problem involving the prediction, evaluation and optimisation of motion under complex physical constraints.

Leading-Edge Roughness (LER) strongly dictates boundary layer transition and performance degradation on an airfoil operating at transitional Reynolds numbers, an aerodynamic regime where shear-layer stability mechanisms remain highly complex.

A significant challenge for autonomous drone landings in unstructured environments is that of reliably detecting and identifying objects in real-time to ensure safety and accuracy of the landing area.

The rapid development of reusable hypersonic space transportation systems has intensified the need for advanced thermal protection technologies capable of withstanding extreme aerodynamic heating conditions encountered during atmospheric re-entry and sustained hypersonic flight.

Estimating the Remaining Useful Life (RUL) of industrial machinery in real-time is now vital for both operational safety and smart resource management.