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Aerospace, Volume 4, Issue 3

September 2017 - 17 articles

Cover Story: In full-scale wind tunnel tests, aerodynamic characteristics of helicopter engine side air intakes are investigated. The experimental data is obtained by testing of a helicopter fuselage section model (complete fuselage in grey, section model displayed in orange and blue). Engine mass flow rates are reproduced to simulate realistic engine operation. Five-hole pressure probe data of the aerodynamic interface plane and surface pressure distributions are applied to evaluate different intake shapes. The optimization potential of retrofit modifications such as a rear spoiler and an inlet guide vane is assessed in reference to a baseline geometry. View the paper here.
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Articles (17)

  • Article
  • Open Access
7 Citations
6,320 Views
11 Pages

Rarefication Effects on Jet Impingement Loads

  • Shiying Cai,
  • Chunpei Cai,
  • Kai Zhang and
  • Jun Li

19 September 2017

Rarefication effects on jet impingement loads are studied by comparing recent new formulas at the collisionless flow limit and numerical simulations. The jet exit size is finite, and can be either planar or round. In the simulations, the jets have di...

  • Article
  • Open Access
18 Citations
13,267 Views
14 Pages

Analysis of Radar and ADS-B Influences on Aircraft Detect and Avoid (DAA) Systems

  • William Semke,
  • Nicholas Allen,
  • Asma Tabassum,
  • Matthew McCrink,
  • Mohammad Moallemi,
  • Kyle Snyder,
  • Evan Arnold,
  • Dawson Stott and
  • Michael G. Wing

18 September 2017

Detect and Avoid (DAA) systems are complex communication and locational technologies comprising multiple independent components. DAA technologies support communications between ground-based and space-based operations with aircraft. Both manned and un...

  • Article
  • Open Access
5 Citations
7,706 Views
20 Pages

11 September 2017

In this paper, we use differential evolution (DE), with best-evolved results refined using a Nelder–Mead optimization, to solve boundary-value complex problems in orbital mechanics relevant to low Earth orbits (LEO). A class of Lambert-type problems...

  • Article
  • Open Access
10 Citations
8,251 Views
10 Pages

Modelling Airport Pollutants Dispersion at High Resolution

  • Claire Sarrat,
  • Sébastien Aubry,
  • Thomas Chaboud and
  • Christine Lac

Local air quality is a major concern for the population regularly exposed to high levels of air pollution. Due mainly to its aircraft engine activities during taxiing and take-off, the airport is often submitted to heterogeneous but important concent...

  • Article
  • Open Access
32 Citations
19,104 Views
22 Pages

Hybrid Electric Aircraft Propulsion Case Study for Skydiving Mission

  • Richard Glassock,
  • Michael Galea,
  • Warren Williams and
  • Tibor Glesk

This paper describes a case study for applying innovative architectures related to electrified propulsion for aircraft. Electric and hybrid electric propulsion for aircraft has gained widespread and significant attention over the past decade. The dri...

  • Article
  • Open Access
22 Citations
9,223 Views
34 Pages

In recent years, global navigation satellite system (GNSS)-based navigation in high earth orbits (HEOs) has become a field of research interest since it can increase the spacecraft’s autonomy, thereby reducing the operating costs. However, the GNSS a...

  • Article
  • Open Access
2 Citations
6,401 Views
12 Pages

The k-out-of-N system is widely applied in several industrial systems. This structure is a part of fault-tolerant systems for which both parallel and series systems are special cases. Because of the importance of industrial systems reliability determ...

  • Article
  • Open Access
14 Citations
7,523 Views
16 Pages

The numerical simulation of multiphysics problems has grown steadily in recent years. This development is due to both the permanent increase of IT resources and the considerable progress made in modeling, mathematical and numerical analysis of many p...

  • Article
  • Open Access
14 Citations
10,026 Views
15 Pages

A detailed numerical investigation of the flow behind a square cylinder at a Reynolds number of 21,400 is conducted to assess the ability of the delayed detached-eddy simulation (DDES) modeling approach to accurately predict the velocity recovery in...

  • Article
  • Open Access
48 Citations
11,627 Views
25 Pages

A Concept for Multi-Criteria Environmental Assessment of Aircraft Trajectories

  • Sigrun Matthes,
  • Volker Grewe,
  • Katrin Dahlmann,
  • Christine Frömming,
  • Emma Irvine,
  • Ling Lim,
  • Florian Linke,
  • Benjamin Lührs,
  • Bethan Owen and
  • Keith Shine
  • + 3 authors

Comprehensive assessment of the environmental aspects of flight movements is of increasing interest to the aviation sector as a potential input for developing sustainable aviation strategies that consider climate impact, air quality and noise issues...

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Aerospace - ISSN 2226-4310