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Aerospace, Volume 8, Issue 3

2021 March - 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
18 Citations
5,715 Views
21 Pages

Transient Dynamic System Behavior of Pressure Actuated Cellular Structures in a Morphing Wing

  • Patrick Meyer,
  • Sebastian Lück,
  • Tobias Spuhler,
  • Christoph Bode,
  • Christian Hühne,
  • Jens Friedrichs and
  • Michael Sinapius

High aspect ratio aircraft have a significantly reduced induced drag, but have only limited installation space for control surfaces near the wingtip. This paper describes a multidisciplinary design methodology for a morphing aileron that is based on...

  • Article
  • Open Access
13 Citations
6,046 Views
20 Pages

Sensitivity Study of Ice Accretion Simulation to Roughness Thermal Correction Model

  • Kevin Ignatowicz,
  • François Morency and
  • Héloïse Beaugendre

The effects of atmospheric icing can be anticipated by Computational Fluid Dynamics (CFD). Past studies show that the convective heat transfer influences the ice accretion and is itself a function of surface roughness. Uncertainty quantification (UQ)...

  • Article
  • Open Access
34 Citations
6,154 Views
21 Pages

This paper presents the application of an active energy management strategy to a hybrid system consisting of a proton exchange membrane fuel cell (PEMFC), battery, and supercapacitor. The purpose of energy management is to control the battery and sup...

  • Article
  • Open Access
18 Citations
5,087 Views
10 Pages

Recent Advances of the BIRALET System about Space Debris Detection

  • Tonino Pisanu,
  • Giacomo Muntoni,
  • Luca Schirru,
  • Pierluigi Ortu,
  • Enrico Urru and
  • Giorgio Montisci

Space debris is internationally recognized as a planetary threat. Efforts to enhance the worldwide radar monitoring networks have been intensified in the last years. Among the new radars employed for the observations, one of the most promising is the...

  • Article
  • Open Access
7 Citations
7,084 Views
25 Pages

The purpose of this study is to analyze the concept of a hybrid apron with a fixed number of parking positions considering the management model influence for the average delay per aircraft and the gaseous emissions generated by aircraft and ground su...

  • Review
  • Open Access
91 Citations
16,738 Views
39 Pages

A Survey on Low-Thrust Trajectory Optimization Approaches

  • David Morante,
  • Manuel Sanjurjo Rivo and
  • Manuel Soler

In this paper, we provide a survey on available numerical approaches for solving low-thrust trajectory optimization problems. First, a general mathematical framework based on hybrid optimal control will be presented. This formulation and their elemen...

  • Article
  • Open Access
7 Citations
3,729 Views
13 Pages

Modular Line-Focused Space Solar Power Satellite

  • Yang Yang,
  • Guanheng Fan,
  • Xiangfei Ji and
  • Mengchen Pei

The Space Solar Power Satellite is an ultra-large space structure, which collects sunlight directly in space and then transmits it into the ground. Since the idea was invented in 1968, scientists around the world have proposed several typical concept...

  • Article
  • Open Access
23 Citations
5,559 Views
17 Pages

Helicopters often operate in dusty sites, ingesting huge amounts of contaminants during landing, take-off, hover-taxi, and ground operations. In specific locations, the downwash of the rotor may spread soil particles from the ground into the environm...

  • Article
  • Open Access
60 Citations
12,720 Views
15 Pages

Experimental Heat Loads for Electrothermal Anti-Icing and De-Icing on UAVs

  • Richard Hann,
  • Adriana Enache,
  • Mikkel Cornelius Nielsen,
  • Bård Nagy Stovner,
  • Jeroen van Beeck,
  • Tor Arne Johansen and
  • Kasper Trolle Borup

Atmospheric in-flight icing on unmanned aerial vehicles (UAVs) is a significant hazard. UAVs that are not equipped with ice protection systems are usually limited to operations within visual line of sight or to weather conditions without icing risk....

  • Article
  • Open Access
2 Citations
5,450 Views
16 Pages

Strength Analysis of Alternative Airframe Layouts of Regional Aircraft on the Basis of Automated Parametrical Models

  • Dmitry V. Vedernikov,
  • Alexander N. Shanygin,
  • Yury S. Mirgorodsky and
  • Mikhail D. Levchenkov

This publication presents the results of complex parametrical strength investigations of typical wings for regional aircrafts obtained by means of the new version of the four-level algorithm (FLA) with the modified module responsible for the analysis...

  • Article
  • Open Access
5 Citations
4,859 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
4,771 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
27 Citations
5,976 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
3,619 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
5,848 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
17 Citations
4,716 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
24 Citations
8,820 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
7,829 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
4,702 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...

  • Article
  • Open Access
13 Citations
4,870 Views
26 Pages

The paper describes the preliminary design of a phasing trajectory in a cislunar environment, where the third body perturbation is considered non-negligible. The working framework is the one proposed by the ESA’s Heracles mission in which a passive t...

  • Article
  • Open Access
20 Citations
5,827 Views
38 Pages

The paper presents the development of a fully-safe, automatic rendezvous strategy between a passive vehicle and an active one orbiting around the Earth–Moon L2 Lagrangian point. This is one of the critical phases of future missions to permanently ret...

  • Article
  • Open Access
3 Citations
7,191 Views
19 Pages

The operational concept of aerodynamic formation flight, also referred to as aircraft wake-surfing for efficiency (AWSE), has high potential in terms of fuel savings and climate impact mitigation. In order to implement this concept, many technologica...

  • Article
  • Open Access
7 Citations
6,138 Views
21 Pages

Numerical Investigation of an Optimized Rotor Head Fairing for the RACER Compound Helicopter in Cruise Flight

  • Patrick Pölzlbauer,
  • Andreas Kümmel,
  • Damien Desvigne and
  • Christian Breitsamter

The present work is part of the Clean Sky 2 project Full-Fairing Rotor Head Aerodynamic Design Optimization (FURADO), which deals with the aerodynamic design optimization of a full-fairing rotor head for the Rapid And Cost-Effective Rotorcraft (RACER...

  • Article
  • Open Access
16 Citations
12,125 Views
24 Pages

The structural safety of solar cells mounted on deployable solar panels in the launch vibration environment is a significant aspect of a successful CubeSat mission. This paper presents a novel highly damped deployable solar panel module that is effec...

  • Review
  • Open Access
66 Citations
15,697 Views
23 Pages

In air traffic control (ATC), speech communication with radio transmission is the primary way to exchange information between the controller and aircrew. A wealth of contextual situational dynamics is embedded implicitly; thus, understanding the spok...

  • Article
  • Open Access
9 Citations
4,441 Views
21 Pages

Because of the light weight and high strength, composite laminates have many advantages in aircraft structures; however, they are frequently subjected to severe dynamic loadings during flight. To understand the dynamic properties of composite laminat...

  • Article
  • Open Access
5 Citations
4,653 Views
11 Pages

Ionizing radiation sources such as Solar Energetic Particles and Galactic Cosmic Radiation may cause unexpected errors in imaging and communication systems of satellites in the Space environment, as reported in the previous literature. In this study,...

  • Article
  • Open Access
17 Citations
3,924 Views
18 Pages

26 February 2021

In the present work, 3D Unsteady Reynolds-Averaged Navier-Stokes (URANS) simulations are performed to investigate the generation and mitigation mechanism of combustion-sustained thermoacoustic instabilities in a modelled swirl combustor. The effects...

  • Article
  • Open Access
51 Citations
10,471 Views
23 Pages

Aircraft Requirements for Sustainable Regional Aviation

  • Dominik Eisenhut,
  • Nicolas Moebs,
  • Evert Windels,
  • Dominique Bergmann,
  • Ingmar Geiß,
  • Ricardo Reis and
  • Andreas Strohmayer

26 February 2021

Recently, the new Green Deal policy initiative was presented by the European Union. The EU aims to achieve a sustainable future and be the first climate-neutral continent by 2050. It targets all of the continent’s industries, meaning aviation must co...

  • Article
  • Open Access
21 Citations
5,455 Views
11 Pages

25 February 2021

Aviation faces increasing pressure not only to reduce fuel burn, and; therefore, CO2 emissions, but also to provide technical solutions for an overall climate impact minimization. To combine both, a concept for the enhancement of an aircraft engine b...

  • Article
  • Open Access
14 Citations
4,160 Views
14 Pages

24 February 2021

Integrating a fan with a boundary layer ingestion (BLI) configuration into an aircraft fuselage can improve propulsion efficiency by utilizing the lower momentum airflow in the boundary layer developed due to the surface drag of the fuselage. As a co...

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Aerospace - ISSN 2226-4310