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Aerospace, Volume 8, Issue 3

March 2021 - 32 articles

Cover Story: The development of future helicopters is subject to the reduction of the environmental impact and the expansion of the flight envelope toward higher cruising speeds. The speed limitation is tackled by the compound helicopter RACER. Due to the high cruise speed, drag mitigation is an important topic. The rotor head represents one of the main drag sources, and the application of rotor head fairings can be an effective drag reduction measure. As part of the RACER full-fairing concept, a new blade-sleeve fairing was aerodynamically optimized for cruise flight. Within the present study, this newly developed blade-sleeve fairing is investigated by numerical flow simulations of an isolated, five-bladed rotor head featuring cyclic pitch movement. View this paper.
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Articles (32)

  • Article
  • Open Access
5 Citations
4,672 Views
25 Pages

On the Handling Qualities of Two Flying Wing Aircraft Configurations

  • Luís M. B. C. Campos and
  • Joaquim M. G. Marques

The coupling of the longitudinal and lateral stability modes of an aeroplane is considered in two cases: (i) weak coupling, when the changes in the frequency and damping of the phugoid, short period, dutch roll, and helical modes are small, i.e., the...

  • Article
  • Open Access
7 Citations
4,633 Views
16 Pages

This work attempts to connect internal flow to the exit flow and supersonic jet mixing in rectangular nozzles with low to high aspect ratios (AR). A series of low and high aspect ratio rectangular nozzles (design Mach number = 1.5) with sharp throats...

  • Article
  • Open Access
26 Citations
5,768 Views
23 Pages

Unmanned Aerial Vehicles (UAVs) undoubtedly pose many security challenges. We need only look to the December 2018 Gatwick Airport incident for an example of the disruption UAVs can cause. In total, 1000 flights were grounded for 36 h over the Christm...

  • Article
  • Open Access
3 Citations
3,535 Views
12 Pages

High-resolution remote sensing images are the key data source for the visual system of a flight simulator for training a qualified pilot. However, due to hardware limitations, it is an expensive task to collect spectral and spatial images at very hig...

  • Article
  • Open Access
9 Citations
5,622 Views
20 Pages

Liquid lubricants are critical to enable long-life operation of high-performance machinery, such as geared actuators employed in robotics. In space applications, actuator gearboxes must operate in low temperatures, where liquid lubricants face inhere...

  • Article
  • Open Access
16 Citations
4,549 Views
16 Pages

Task Planning for Multiple-Satellite Space-Situational-Awareness Systems

  • Yutao Chen,
  • Guoqing Tian,
  • Junyou Guo and
  • Jie Huang

Space situational awareness (SSA) plays an important role in maintaining space advantages. Task planning is one of the key technologies in SSA to allocate multiple tasks to multiple satellites, so that a satellite may be allocated to supervise multip...

  • Article
  • Open Access
23 Citations
8,373 Views
35 Pages

Testing of untethered subscale models, often referred to as subscale flight testing, has traditionally had a relatively minor, yet relevant use in aeronautical research and development. As recent advances in electronics, rapid prototyping and unmanne...

  • Article
  • Open Access
19 Citations
7,469 Views
28 Pages

The envisioned introduction of autonomous Small Unmanned Aircraft Systems (sUAS) into low-altitude urban airspace necessitates high levels of system safety. Despite increased system autonomy, humans will most likely remain an essential component in a...

  • Article
  • Open Access
16 Citations
4,425 Views
22 Pages

Background Pressure Effects on the Performance of a 20 kW Magnetically Shielded Hall Thruster Operating in Various Configurations

  • Antonio Piragino,
  • Farbod Faraji,
  • Maryam Reza,
  • Eugenio Ferrato,
  • Annalisa Piraino and
  • Tommaso Andreussi

The paper reports the characterization results of a 20 kW-class magnetically shielded Hall thruster in three different configurations and operating with a centrally mounted cathode. The characterization was carried out at two different pumping speeds...

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Aerospace - ISSN 2226-4310