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Aerospace, Volume 8, Issue 1

2021 January - 23 articles

Cover Story: Commonly, the modelling of pollutant emissions from aeroengines is limited to the combustion chamber, as the composition at its outlet is considered “chemically frozen”. However, this assumption is not necessarily valid, especially with the increasing turbine inlet temperatures and operating pressures. Simulations were performed to analyse NOx and CO through the high-pressure turbine stator. Progression of relevant reactions continues within the stator. Reaction rates are correlated with flow structures for the cruise condition, especially in the near-wall flow and the blade wakes. Interestingly, at the higher operating pressure and temperature during take-off, reactions are dependent on the residence time instead. View this paper.
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Articles (23)

  • Review
  • Open Access
195 Citations
34,548 Views
30 Pages

Electric Propulsion Methods for Small Satellites: A Review

  • Dillon O’Reilly,
  • Georg Herdrich and
  • Darren F. Kavanagh

18 January 2021

Over 2500 active satellites are in orbit as of October 2020, with an increase of ~1000 smallsats in the past two years. Since 2012, over 1700 smallsats have been launched into orbit. It is projected that by 2025, there will be 1000 smallsats launched...

(This article belongs to the Special Issue Electric Propulsion)
  • Article
  • Open Access
26 Citations
15,625 Views
20 Pages

17 January 2021

Sounding balloons, available at very low cost from commercial vendors and operable with minimal training, have an excellent potential as testing platforms in the near-space environment. The work reported here was motivated by the need to perform an e...

  • Article
  • Open Access
7 Citations
3,956 Views
16 Pages

Numerical Analysis of Flow across Brush Elements Based on a 2-D Staggered Tube Banks Model

  • Xiaolei Song,
  • Meihong Liu,
  • Xiangping Hu,
  • Xueliang Wang,
  • Taohong Liao and
  • Junfeng Sun

15 January 2021

In order to improve efficiency in turbomachinery, brush seal replaces labyrinth seals widely in the secondary air system. A 2-d staggered tube bank model is adopted to simulate the gas states and the pressure character in brush seal, and computationa...

(This article belongs to the Section Aeronautics)
  • Review
  • Open Access
151 Citations
27,919 Views
21 Pages

15 January 2021

Current research trends have advanced the use of “green propellants” on a wide scale for spacecraft in various space missions; mainly for environmental sustainability and safety concerns. Small satellites, particularly micro and nanosatel...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
18 Citations
8,382 Views
15 Pages

The Efficacy of Operational Bird Strike Prevention

  • Isabel C. Metz,
  • Joost Ellerbroek,
  • Thorsten Mühlhausen,
  • Dirk Kügler,
  • Stefan Kern and
  • Jacco M. Hoekstra

14 January 2021

Involving air traffic controllers and pilots into the bird strike prevention process is considered an essential step to increase aviation and avian safety. Prior to implementing operational measures such as real-time warning systems, it is vital to e...

(This article belongs to the Collection Air Transportation—Operations and Management)
  • Article
  • Open Access
17 Citations
5,287 Views
16 Pages

14 January 2021

Deep reinforcement learning is a promising method for training a nonlinear attitude controller for fixed-wing unmanned aerial vehicles. Until now, proof-of-concept studies have demonstrated successful attitude control in simulation. However, detailed...

  • Article
  • Open Access
21 Citations
5,061 Views
16 Pages

Effect of Increased Cabin Recirculation Airflow Fraction on Relative Humidity, CO2 and TVOC

  • Victor Norrefeldt,
  • Florian Mayer,
  • Britta Herbig,
  • Ria Ströhlein,
  • Pawel Wargocki and
  • Fang Lei

13 January 2021

In the CleanSky 2 ComAir study, subject tests were conducted in the Fraunhofer Flight Test Facility cabin mock-up. This mock-up consists of the front section of a former in-service A310 hosting up to 80 passengers. In 12 sessions the outdoor/recircul...

(This article belongs to the Special Issue 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens)
  • Article
  • Open Access
72 Citations
18,914 Views
65 Pages

Proof of Concept Study for Fuselage Boundary Layer Ingesting Propulsion

  • Arne Seitz,
  • Anaïs Luisa Habermann,
  • Fabian Peter,
  • Florian Troeltsch,
  • Alejandro Castillo Pardo,
  • Biagio Della Corte,
  • Martijn van Sluis,
  • Zdobyslaw Goraj,
  • Mariusz Kowalski and
  • Guido Wortmann
  • + 3 authors

13 January 2021

Key results from the EU H2020 project CENTRELINE are presented. The research activities undertaken to demonstrate the proof of concept (technology readiness level—TRL 3) for the so-called propulsive fuselage concept (PFC) for fuselage wake-fill...

(This article belongs to the Special Issue 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens)
  • Article
  • Open Access
15 Citations
5,714 Views
18 Pages

Climate Impact Mitigation Potential of Formation Flight

  • Tobias Marks,
  • Katrin Dahlmann,
  • Volker Grewe,
  • Volker Gollnick,
  • Florian Linke,
  • Sigrun Matthes,
  • Eike Stumpf,
  • Majed Swaid,
  • Simon Unterstrasser and
  • Clemens Zumegen
  • + 1 author

The aerodynamic formation flight, which is also known as aircraft wake-surfing for efficiency (AWSE), enables aircraft to harvest the energy inherent in another aircraft’s wake vortex. As the thrust of the trailing aircraft can be reduced durin...

(This article belongs to the Special Issue Selected Papers from 3rd ECATS Conference on Making Aviation Environmentally Sustainable)
  • Article
  • Open Access
17 Citations
8,587 Views
19 Pages

Quasi-3D Aerodynamic Analysis Method for Blended-Wing-Body UAV Configurations

  • Pericles Panagiotou,
  • Thomas Dimopoulos,
  • Stylianos Dimitriou and
  • Kyros Yakinthos

The current study presents a low-fidelity, quasi-3D aerodynamic analysis method for Blended-Wing-Body (BWB) Unmanned Aerial Vehicle (UAV) configurations. A tactical BWB UAV experimental prototype is used as a reference platform. The method utilizes 2...

  • Article
  • Open Access
6 Citations
4,608 Views
19 Pages

Evolution of Emission Species in an Aero-Engine Turbine Stator

  • André A. V. Perpignan,
  • Stella Grazia Tomasello and
  • Arvind Gangoli Rao

Future energy and transport scenarios will still rely on gas turbines for energy conversion and propulsion. Gas turbines will play a major role in energy transition and therefore gas turbine performance should be improved, and their pollutant emissio...

(This article belongs to the Special Issue Progress in Jet Engine Technology II)
  • Article
  • Open Access
8 Citations
5,780 Views
19 Pages

This work focuses its attention on possibilities to enhance the stability of an axial compressor using a casing treatment technique. Circumferential grooves machined into the case are considered and their performances evaluated using three-dimensiona...

(This article belongs to the Special Issue Progress in Jet Engine Technology II)
  • Correction
  • Open Access
2,867 Views
1 Page

30 December 2020

The authors regret that this paper [1] contains typographical errors in the sentence between Equation (16) and Equation (17), as well as in Equations (18), (20), (21), (34), (36) and (37), with respect to the point that they use the wrong notations t...

(This article belongs to the Special Issue Innovative Space Mission Analysis and Design for Space Sciences, Earth Observation, Global Change, Space Weather)
  • Article
  • Open Access
8 Citations
8,735 Views
28 Pages

Novel 3U Stand-Alone CubeSat Architecture for Autonomous Near Earth Asteroid Fly-By

  • Stefano Casini,
  • Iosto Fodde,
  • Bert Monna,
  • Angelo Cervone and
  • Eberhard Gill

30 December 2020

The purpose of this work is to present a novel CubeSat architecture, aimed to explore Near Earth Asteroids. The fast growth in small satellite commercial-off-the-shelf technologies, which characterized the last decade of space industry, is exploited...

(This article belongs to the Special Issue Small Satellite Technologies and Mission Concepts)
  • Article
  • Open Access
14 Citations
10,613 Views
31 Pages

30 December 2020

Amphibious aircraft designers face challenges to improve takeoffs and landings on both water and land, with water-takeoffs being relatively more complex for analyses. Reducing the water-takeoff distance via the use of hydrofoils was a subject of inte...

(This article belongs to the Special Issue Aircraft Design (SI-2/2020))
  • Article
  • Open Access
6 Citations
5,168 Views
25 Pages

29 December 2020

Large-amplitude excitations need to be considered for gust load analyses of transport aircraft in cruise flight conditions. Nonlinear amplitude effects in transonic flow are, however, only marginally taken into account. The present work aims at closi...

  • Article
  • Open Access
4 Citations
4,754 Views
12 Pages

28 December 2020

In this concept-proof study, a preform-based RTM (Resin Transfer Molding) process is presented that is characterized by first pre-loading the solid curing agent onto the preform, and then injecting the liquid nonreactive resin with an intrinsically l...

(This article belongs to the Special Issue Advances in Aerospace Sciences and Technology)
  • Article
  • Open Access
11 Citations
5,294 Views
20 Pages

28 December 2020

The problem that two cooperative missiles intercept a maneuvering target while imposing a desired relative geometry is investigated in the paper. Firstly, a three-dimensional (3D) estimation model for cooperative target tracking is proposed and the o...

  • Article
  • Open Access
34 Citations
5,363 Views
18 Pages

LEO Object’s Light-Curve Acquisition System and Their Inversion for Attitude Reconstruction

  • Fabrizio Piergentili,
  • Gaetano Zarcone,
  • Leonardo Parisi,
  • Lorenzo Mariani,
  • Shariar Hadji Hossein and
  • Fabio Santoni

23 December 2020

In recent years, the increase in space activities has brought the space debris issue to the top of the list of all space agencies. The fact of there being uncontrolled objects is a problem both for the operational satellites in orbit (avoiding collis...

  • Article
  • Open Access
11 Citations
8,827 Views
20 Pages

23 December 2020

The purpose of this paper is to investigate the influence of the engine position and mass as well as the pylon stiffness on the aeroelastic stability of a long-range wide-body transport aircraft. As reference configuration, DLR’s (German Aerosp...

(This article belongs to the Special Issue Aeroelasticity, Volume II)
  • Article
  • Open Access
83 Citations
15,684 Views
22 Pages

Design and Optimization of Ram Air–Based Thermal Management Systems for Hybrid-Electric Aircraft

  • Hagen Kellermann,
  • Michael Lüdemann,
  • Markus Pohl and
  • Mirko Hornung

23 December 2020

Ram air–based thermal management systems (TMS) are investigated herein for the cooling of future hybrid-electric aircraft. The developed TMS model consists of all components required to estimate the impacts of mass, drag, and fuel burn on the a...

(This article belongs to the Special Issue 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens)
  • Article
  • Open Access
43 Citations
12,482 Views
16 Pages

22 December 2020

Manufacturing costs, along with operational performance, are among the major factors determining the selection of the propulsion system for unmanned aerial vehicles (UAVs), especially for aerial targets and cruise missiles. In this paper, the design...

(This article belongs to the Special Issue 10th EASN International Conference on Innovation in Aviation & Space to the Satisfaction of the European Citizens)
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Aerospace - ISSN 2226-4310