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Aerospace, Volume 6, Issue 5

May 2019 - 13 articles

Cover Story: Modern aircraft engines must operate at ever-higher temperatures, pressures, and rotational speeds, in order to increase power and improve efficiency. This creates an extreme operating environment for engine blades, which are the most frequently rejected part during engine maintenance. Their failure can lead to severe unairworthiness and fatalities. Hence, it is important to identify and precisely define all defects. This paper provides a comprehensive and illustrated list of engine blade defects, as well as standardized defect terminology, which currently does not exist in the aviation industry. It proposes a taxonomy for both engine blade defects and root causes, and an ontology that shows their correlations. View this paper
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Articles (13)

  • Article
  • Open Access
17 Citations
6,596 Views
23 Pages

Solar Module Integrated Converters as Power Generator in Small Spacecrafts: Design and Verification Approach

  • Jesus Gonzalez-Llorente,
  • Aleksander A. Lidtke,
  • Ken Hatanaka,
  • Ryo Kawauchi and
  • Kei-Ichi Okuyama

As small satellites are becoming more widespread for new businesses and applications, the development time, failure rate and cost of the spacecraft must be reduced. One of the systems with the highest cost and the most frequent failure in the satelli...

  • Article
  • Open Access
6 Citations
6,448 Views
17 Pages

Flow within the space between the rotor and stator of a turbine disk, and an area referred to as the rim seal cavity, develops azimuthal velocity component from the rotor disk. The fluid within develops unsteady structures that move at a fraction of...

  • Article
  • Open Access
12 Citations
5,519 Views
20 Pages

The possibility of realizing full electric or hybrid electric propulsion for aircraft has been considered due to the constant growth in the use of electric technologies in aircraft and the availability of high-power-density electrical machines and co...

  • Article
  • Open Access
21 Citations
8,599 Views
19 Pages

Accurate 2-D Modelling of Transonic Compressor Cascade Aerodynamics

  • Tommaso Piovesan,
  • Andrea Magrini and
  • Ernesto Benini

Modern aeronautic fans are characterised by a transonic flow regime near the blade tip. Transonic cascades enable higher pressure ratios by a complex system of shockwaves arising across the blade passage, which has to be correctly reproduced in order...

  • Feature Paper
  • Review
  • Open Access
27 Citations
9,228 Views
29 Pages

The computational fluid dynamics of hybrid rocket internal ballistics is becoming a key tool for reducing the engine operation uncertainties and development cost as well as for improving experimental data analysis. Nevertheless, its application still...

  • Article
  • Open Access
36 Citations
13,334 Views
34 Pages

In this study, the on-going research into the improvement of micro-gas turbine propulsion system performance and the suitability for its application as propulsion systems for small tactical UAVs (<600 kg) is investigated. The study is focused arou...

  • Article
  • Open Access
17 Citations
7,817 Views
17 Pages

Engineering Methodology for Student-Driven CubeSats

  • Abdulaziz Alanazi and
  • Jeremy Straub

CubeSats are widely used by universities and research institutions all over the world. Their popularity is generally attributed to the use of low-cost components, free student labor and simple design. They have been shown to encourage Science, Techno...

  • Article
  • Open Access
21 Citations
9,579 Views
14 Pages

Innovating the Maintenance Repair and Overhaul Phase through Digitalization

  • Marco Esposito,
  • Mariangela Lazoi,
  • Antonio Margarito and
  • Lorenzo Quarta

Improving processes in a company starts from a deep knowledge of the current context, of the needs for improvement and of the objectives to be satisfied. Sometimes, traditional processes can benefit from a techno-organizational innovation that change...

  • Article
  • Open Access
12 Citations
5,971 Views
15 Pages

The presence of cut-outs within thin-walled shell structures is unavoidable, holes being needed for the passage of electrical cables, fuel, or just to reduce the weight of the components. Nevertheless, the high stress concentration can lead to a prem...

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Aerospace - ISSN 2226-4310