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Aerospace, Volume 6, Issue 8

August 2019 - 8 articles

Cover Story: Thermodynamic cycle analysis tools play a critical role in evaluating the performance of gas turbine engines, but they have traditionally been used as stand-alone codes. As propulsion systems become more integrated with the vehicle design, the propulsion models need to become more integrated as well. This research developed a new cycle analysis library, called pyCycle, to enable multidisciplinary gradient-based design optimization of engines for these new vehicle concepts. pyCycle provides efficient analytic derivatives for propulsion models built with it, leading to seven times faster optimization compared to existing tools. View this paper.
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Articles (8)

  • Article
  • Open Access
13 Citations
13,758 Views
17 Pages

Adelis-SAMSON is a nano-satellite mission aimed at performing geo-location of target signals on Earth using a tight three-satellite formation in space. To maintain formation, each nano-satellite is equipped with a cold gas propulsion system. The desi...

  • Article
  • Open Access
7 Citations
8,646 Views
19 Pages

Conventional fixed wing aircraft require a selection of certain thickness of skin material that guarantees structural strength for aerodynamic loadings in various flight modes. However, skin structures of morphing wings are expected to be flexible as...

  • Article
  • Open Access
18 Citations
5,986 Views
15 Pages

Design and Testing of a Paraffin-Based 1000 N HRE Breadboard

  • Francesco Battista,
  • Daniele Cardillo,
  • Manrico Fragiacomo,
  • Giuseppe Daniele Di Martino,
  • Stefano Mungiguerra and
  • Raffaele Savino

The paper presents some relevant achievements in hybrid rocket propulsion carried out by the Italian Aerospace Research Centre. On the basis of the experimental results obtained on a 200 N thrust class engine, a 1000 N class breadboard, fed with gase...

  • Article
  • Open Access
23 Citations
6,717 Views
26 Pages

Modeling of High Density Polyethylene Regression Rate in the Simulation of Hybrid Rocket Flowfields

  • Daniele Bianchi,
  • Giuseppe Leccese,
  • Francesco Nasuti,
  • Marcello Onofri and
  • Carmine Carmicino

Numerical analysis of hybrid rocket internal ballistics is carried out with a Reynolds-averaged Navier–Stokes solver integrated with a customized gas–surface interaction wall boundary condition and coupled with a radiation code based on t...

  • Article
  • Open Access
81 Citations
17,181 Views
36 Pages

Aviation researchers are increasingly focusing on unconventional vehicle designs with tightly integrated propulsion systems to improve overall aircraft performance and reduce environmental impact. Properly analyzing these types of vehicle and propuls...

  • Article
  • Open Access
10 Citations
5,699 Views
21 Pages

Numerical simulations are crucial for fast and accurate estimations of the flow characteristics in many engineering applications such as atmospheric boundary layers around buildings, external aerodynamics around vehicles, and pollutant dispersion. In...

  • Article
  • Open Access
10 Citations
13,330 Views
24 Pages

The presented aircraft is capable of alternating between two singular working points by folding the exterior surfaces of the wing underneath the interior surfaces. This allows for a significant change in wingspan, lift surfaces, aspect ratio and airf...

  • Editorial
  • Open Access
4,246 Views
2 Pages

This Special Issue contains selected papers from works presented at the 8th EASN–CEAS (European Aeronautics Science Network–Council of European Aerospace Societies) Workshop on Manufacturing for Growth and Innovation, which was held in Gl...

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Aerospace - ISSN 2226-4310