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Aerospace, Volume 6, Issue 2

February 2019 - 15 articles

Cover Story: The development of new aviation technologies typically involves a high risk, which slows down innovation. Unmanned aerial systems (UAS) like the e-Genius-Mod can be useful tools in aircraft design to help to promote innovative ideas and technologies. A UAS can enable the in-flight demonstration and validation of new technologies with a scaled prototype in a relevant environment at an early stage, considerably mitigating development risks. E-Genius-Mod is a scaled version of the University of Stuttgart’s electrically powered e-Genius which was built to investigate the similitude requirements between scale and full-scale testing and serves as a test platform for innovative technologies. View this paper
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Articles (15)

  • Article
  • Open Access
24 Citations
7,300 Views
25 Pages

22 February 2019

System identification from measured flight test data was conducted using the X-56A aeroelastic demonstrator to identify a longitudinal flight dynamics model that included the short period, first symmetric wing bending, and first symmetric wing torsio...

  • Article
  • Open Access
12 Citations
8,184 Views
34 Pages

Process Development for Integrated and Distributed Rotorcraft Design

  • Peter Weiand,
  • Michel Buchwald and
  • Dominik Schwinn

21 February 2019

The German Aerospace Center is currently developing a new design environment for rotorcraft, which combines sizing, simulation and evaluation tasks into one toolbox. The complete environment applies distributed computation on the servers of the vario...

  • Article
  • Open Access
15 Citations
8,427 Views
22 Pages

Static and Dynamic Performance of a Morphing Trailing Edge Concept with High-Damping Elastomeric Skin

  • Maurizio Arena,
  • Christof Nagel,
  • Rosario Pecora,
  • Oliver Schorsch,
  • Antonio Concilio and
  • Ignazio Dimino

19 February 2019

Nature has many striking examples of adaptive structures: the emulation of birds’ flight is the true challenge of a morphing wing. The integration of increasingly innovative technologies, such as reliable kinematic mechanisms, embedded servo-ac...

  • Article
  • Open Access
3 Citations
5,319 Views
21 Pages

15 February 2019

An extant bird resorts to flapping and running along its take-off run to generate lift and thrust in order to reach the minimum required wing velocity speed required for lift-off. This paper introduces the replication hypothesis that posits that the...

  • Article
  • Open Access
11 Citations
9,312 Views
14 Pages

Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft

  • Evgeny Dubovikov,
  • Danil Fomin,
  • Natalia Guseva,
  • Ivan Kondakov,
  • Evgeny Kruychkov,
  • Ivan Mareskin and
  • Alexander Shanygin

14 February 2019

For this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufa...

  • Article
  • Open Access
18 Citations
8,394 Views
20 Pages

14 February 2019

The airworthiness certification of aerospace cyber-physical systems traditionally relies on the probabilistic safety assessment as a standard engineering methodology to quantify the potential risks associated with faults in system components. This pa...

  • Review
  • Open Access
18 Citations
7,909 Views
14 Pages

Innovative Scaled Test Platform e-Genius-Mod—Scaling Methods and Systems Design

  • Dominique Paul Bergmann,
  • Jan Denzel,
  • Asmus Baden,
  • Lucas Kugler and
  • Andreas Strohmayer

14 February 2019

Future aircraft design highly depends on the successful implementation of new technologies. However, the gap between conventional designs and new visions often comes with a high financial risk. This significantly complicates the integration of innova...

  • Article
  • Open Access
8 Citations
5,746 Views
14 Pages

13 February 2019

Future power equipment tends to take hydrogen or middle/low heat-value syngas as fuel for low emission. The heat transfer of a film-cooled turbine blade shall be influenced more by radiation. Its characteristic of conjugate heat transfer is studied e...

  • Article
  • Open Access
6 Citations
5,433 Views
17 Pages

Mitigation of Impact Damage with Self-Healing and Anti-Sloshing Materials in Aerospace Fuel Tanks

  • Gerardus Janszen,
  • Gabriele Capezzera,
  • Antonio Mattia Grande and
  • Luca Di Landro

12 February 2019

In this study, self-healing and anti-sloshing materials are investigated for mitigation of impact-induced damage. The integration of these systems, for the prevention of fire or explosion due to impact or bullet damage, may significantly improve the...

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Aerospace - ISSN 2226-4310Creative Common CC BY license