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Aerospace, Volume 6, Issue 10

2019 October - 13 articles

Cover Story: The application of morphing wing devices can bring several benefits in terms of aircraft performance. Within the framework of AirGreen 2, a European research project running along the CleanSky2 platform, a safety-driven design of an adaptive winglet was created through the examination of potential hazards resulting from operational faults, such as actuation jamming or structural failures. The main goal was to verify whether the morphing winglet systems could comply with the standards of civil flight safety regulations (EASA CS-25) and airworthiness requirements, especially from an aeroelastic stability standpoint. Fault trees were finally developed to assess the compliance of the system to the quantitative safety requirements deriving from the fault and hazard analyses (FHAs). View this paper.
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Articles (13)

  • Article
  • Open Access
4 Citations
7,535 Views
25 Pages

21 October 2019

One of the main limitations of linearity assumptions in airfoil’s aero-elastic problems is the inability to predict the system behavior after starting the instability. In reality, nonlinearities may prevent the amplitudes from going to infinity...

  • Article
  • Open Access
21 Citations
8,149 Views
16 Pages

9 October 2019

The Anti-icing Materials International Laboratory (AMIL) has been testing SAE AMS1424 and AMS1428 ground de-icing/anti-icing fluids for more than 30 years. With the introduction of new surface coatings and their investigation as potential passive ice...

  • Article
  • Open Access
27 Citations
8,991 Views
20 Pages

Investigation of Additively Manufactured Wind Tunnel Models with Integrated Pressure Taps for Vortex Flow Analysis

  • Matteo Moioli,
  • Christopher Reinbold,
  • Kaare Sørensen and
  • Christian Breitsamter

8 October 2019

Wind tunnel models are traditionally machined from high-quality metal material; this condition reduces the possibility to test different geometric variations or models as it corresponds to incremental cost. In the last decade, the quality of additive...

(This article belongs to the Special Issue Design and Analysis of Wind-Tunnel Models and Fluidic Measurements)
  • Article
  • Open Access
27 Citations
8,398 Views
14 Pages

SPH-FEM Design of Laminated Plies under Bird-Strike Impact

  • Yadong Zhou,
  • Youchao Sun and
  • Tianlin Huang

7 October 2019

Composite laminates can potentially reduce the weight of aircrafts; however, they are subjected to bird strike hazards in civil aviation. To handle their nonlinear dynamic behaviour, in this study, the impact damage of composite laminates were numeri...

(This article belongs to the Special Issue Crashworthiness Design for Aviation Safety)
  • Article
  • Open Access
33 Citations
19,964 Views
30 Pages

2 October 2019

Background—The inspection of aircraft parts is critical, as a defective part has many potentially adverse consequences. Faulty parts can initiate a system failure on an aircraft, which can lead to aircraft mishap if not well managed and has the...

(This article belongs to the Special Issue Civil and Military Airworthiness: Recent Developments and Challenges)
  • Article
  • Open Access
18 Citations
13,124 Views
21 Pages

Morphing Wing Droop Nose with Large Deformation: Ground Tests and Lessons Learned

  • Srinivas Vasista,
  • Johannes Riemenschneider,
  • Ralf Keimer,
  • Hans Peter Monner,
  • Felix Nolte and
  • Peter Horst

2 October 2019

A design for a new high lift system that features a morphing wing leading edge “droop nose” has the potential to generate high lift coefficients whilst mitigating airframe noise emissions. This seamless, continuous, and stepless flexible...

(This article belongs to the Special Issue Aeronautical Systems for Flow Control)
  • Article
  • Open Access
21 Citations
11,052 Views
30 Pages

1 October 2019

Hybrid laminar flow control or HLFC design is a complex and multi-disciplinary process, which demands a thorough understanding of all aspects from a global systems viewpoint. The objective of the paper is to present a preliminary design of important...

(This article belongs to the Special Issue Aeronautical Systems for Flow Control)
  • Article
  • Open Access
6 Citations
11,493 Views
22 Pages

27 September 2019

An increasing number of aircraft is equipped with wing tip devices, which either are installed by the aircraft manufacturer at the production line or are retrofitted after the delivery of the aircraft to its operator. The installation of wing tip dev...

  • Article
  • Open Access
35 Citations
16,013 Views
38 Pages

Design, Implementation, and Operation of a Small Satellite Mission to Explore the Space Weather Effects in LEO

  • Isai Fajardo,
  • Aleksander A. Lidtke,
  • Sidi Ahmed Bendoukha,
  • Jesus Gonzalez-Llorente,
  • Rafael Rodríguez,
  • Rigoberto Morales,
  • Dmytro Faizullin,
  • Misuzu Matsuoka,
  • Naoya Urakami and
  • Kei-ichi Okuyama
  • + 14 authors

27 September 2019

Ten-Koh is a 23.5 kg, low-cost satellite developed to conduct space environment effects research in low-Earth orbit (LEO). Ten-Koh was developed primarily by students of the Kyushu Institute of Technology (Kyutech) and launched on 29 October 2018 on-...

(This article belongs to the Special Issue Innovative Space Mission Analysis and Design for Space Sciences, Earth Observation, Global Change, Space Weather)
  • Article
  • Open Access
20 Citations
7,667 Views
34 Pages

24 September 2019

The correct behavior of spacecraft components is the foundation of unhindered mission operation. However, no technical system is free of wear and degradation. A malfunction of one single component might significantly alter the behavior of the whole s...

  • Article
  • Open Access
11 Citations
6,529 Views
12 Pages

In-Situ Testing of a Multi-Band Software-Defined Radio Platform in a Mixed-Field Irradiation Environment

  • Jan Budroweit,
  • Steffen Mueller,
  • Mattis Jaksch,
  • Rubén Garcia Alía,
  • Andrea Coronetti and
  • Alexander Koelpin

24 September 2019

This paper presents an in-situ test concept for a multi-band software-defined radio (SDR) platform in a mixed-field radiation environment. Special focus is given to the complex automated test setup with respect to the requirements of the irradiation...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
44 Citations
16,155 Views
20 Pages

20 September 2019

This paper proposes data-driven queuing models and solutions to reduce arrival time delays originating from aircraft arrival processing bottlenecks at Tokyo International Airport. A data-driven analysis was conducted using two years of radar tracks a...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
33 Citations
8,239 Views
19 Pages

Aeroelastic Assessments and Functional Hazard Analysis of a Regional Aircraft Equipped with Morphing Winglets

  • Maria Chiara Noviello,
  • Ignazio Dimino,
  • Antonio Concilio,
  • Francesco Amoroso and
  • Rosario Pecora

20 September 2019

The application of morphing wing devices can bring several benefits in terms of aircraft performance, as the current literature shows. Within the scope of Clean Sky 2 AirGreen 2 European project, the authors provided a safety-driven design of an adap...

(This article belongs to the Special Issue Adaptive/Smart Structures and Multifunctional Materials in Aerospace)
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Aerospace - ISSN 2226-4310