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Aerospace, Volume 8, Issue 6

2021 June - 25 articles

Cover Story: The ingestion of dust particles by aero-engines results in reduced efficiency, performance and engine life. Predicting the rate at which this deterioration occurs requires knowledge of the engine operating state and particle properties, the latter of which are often unknown or poorly constrained. Coupling reduced-order component damage models with engine performance predictions allows a Monte Carlo analysis to be undertaken and performance degradation rates to be predicted with calculated levels of confidence. The coupled approach can also be used to predict the uncertain dust properties by correlation with measured engine performance degradation. This will ultimately enable the use of the model to predict future engine degradation and, therefore, aid progress towards more predictive maintenance strategies. View this paper.
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Articles (25)

  • Article
  • Open Access
20 Citations
9,610 Views
26 Pages

Green propellants are currently considered as enabling technology that is revolutionizing the development of high-performance space propulsion, especially for small-sized spacecraft. Modern space missions, either in LEO or interplanetary, require rel...

  • Article
  • Open Access
16 Citations
3,991 Views
18 Pages

Remaining-useful-life prognostics for aircraft components are central for efficient and robust aircraft maintenance. In this paper, we propose an end-to-end approach to obtain online, model-based remaining-useful-life prognostics by learning from clu...

  • Article
  • Open Access
15 Citations
5,320 Views
21 Pages

Fixed Wing Aircraft Automatic Landing with the Use of a Dedicated Ground Sign System

  • Bartłomiej Brukarczyk,
  • Dariusz Nowak,
  • Piotr Kot,
  • Tomasz Rogalski and
  • Paweł Rzucidło

The paper presents automatic control of an aircraft in the longitudinal channel during automatic landing. There are two crucial components of the system presented in the paper: a vision system and an automatic landing system. The vision system proces...

  • Article
  • Open Access
2 Citations
4,044 Views
13 Pages

Effect of a Circular Slot on Hybrid Airship Aerodynamic Characteristics

  • Sekar Mano,
  • RadhaKrishnan Ajay Sriram,
  • Ganesan Vinayagamurthy,
  • Subramania Nadaraja Pillai,
  • Amjad Ali Pasha,
  • Dwarshala Siva Krishna Reddy and
  • Mustafa Mutiur Rahman

This numerical study reports the aerodynamic properties of a hybrid airship. The hybrid airships were designed by combining two semi-ellipsoids with a semi-discoid as the base model. From the base model, three different geometrics were identified to...

  • Article
  • Open Access
25 Citations
6,017 Views
23 Pages

Although the application of new wake turbulence categories, the so-called “RECAT (wake turbulence category re-categorization)”, will realize lower aircraft separation minima and directly increase runway throughput, the impacts of increasing arrival t...

  • Article
  • Open Access
65 Citations
11,016 Views
29 Pages

The feasibility of regional electric aviation to reduce environmental impact highly depends on technological advancements of energy storage techniques, available battery energy density, and high-power electric motor technologies. However, novel airfr...

  • Article
  • Open Access
7,158 Views
9 Pages

The current study investigates the application of statistical methods to flight, which have been used in science over time to understand complex physical and mathematical systems by using randomly generated numbers as input into those systems to gene...

  • Article
  • Open Access
11 Citations
5,334 Views
22 Pages

Discretionary activities such as retail, food, and beverages generate a significant amount of non-aeronautical revenue within the aviation industry. However, they are rarely taken into account in computational airport terminal models. Since discretio...

  • Article
  • Open Access
6 Citations
6,144 Views
17 Pages

Software-defined radio (SDR) devices have made a massive contribution to communication systems by reducing the cost and development time for radio frequency (RF) designs. SDRs opened the gate to programmers and enabled them to increase the capabiliti...

  • Article
  • Open Access
6 Citations
5,502 Views
20 Pages

The Effect of Manufacturing Quality on Rocket Precision

  • Zvonko Trzun,
  • Milan Vrdoljak and
  • Hrvoje Cajner

The effect of manufacturing quality on rocket impact point dispersion is analyzed. The approach presented here applies to any type of rocket. Here, manufacturing quality is demonstrated for the unguided rocket, and by simulating four typical manufact...

  • Article
  • Open Access
5 Citations
5,473 Views
18 Pages

In this study, a real-time engine model and a test bench were developed to verify the performance of the EECU (electronic engine control unit) of a turbofan engine. The target engine is a DGEN 380 developed by the Price Induction company. The functio...

  • Article
  • Open Access
20 Citations
4,417 Views
11 Pages

Deflected control surfaces can be used as variable camber control in different flight conditions, and a convex corner resembles a simplified configuration for the upper surface. This experimental study determines the presence of passive vortex genera...

  • Article
  • Open Access
8 Citations
3,396 Views
17 Pages

Aiming at the task planning and scheduling problem of space object detection LEO constellation (SODLC) for detecting space objects in deep space background, a method of SODLC task satellite selection based on observation window projection analysis is...

  • Article
  • Open Access
3 Citations
5,371 Views
20 Pages

Paris Charles de Gaulle Airport was the second European airport in terms of traffic in 2019, having transported 76.2 million passengers. Its large infrastructures include four runways, a large taxiway network, and 298 aircraft parking stands (131 con...

  • Article
  • Open Access
55 Citations
14,459 Views
20 Pages

The problem of flight delay prediction is approached most often by predicting a delay class or value. However, the aviation industry can benefit greatly from probabilistic delay predictions on an individual flight basis, as these give insight into th...

  • Article
  • Open Access
7,912 Views
22 Pages

From the Martian Surface to Its Low Orbit in a Reusable Single-Stage Vehicle—Charon

  • Jérémie Gaffarel,
  • Afrasiab Kadhum,
  • Mohammad Fazaeli,
  • Dimitrios Apostolidis,
  • Menno Berger,
  • Lukas Ciunaitis,
  • Wieger Helsdingen,
  • Lasse Landergren,
  • Mateusz Lentner and
  • Marc Naeije
  • + 2 authors

With Mars colonisation becoming a reality for the near future, it is of importance to analyse how crew and cargo can be transported between Earth and a colony on Mars. This article is a feasibility and design study of a launch vehicle whose mission i...

  • Article
  • Open Access
5 Citations
5,720 Views
19 Pages

A Web-Based Decision Support System for Aircraft Dispatch and Maintenance

  • Hemmo Koornneef,
  • Wim J. C. Verhagen and
  • Richard Curran

Aircraft dispatch involves determining the optimal dispatch option when an aircraft experiences an unexpected failure. Currently, maintenance technicians at the apron have limited access to support information and finding the right information in ext...

  • Article
  • Open Access
11 Citations
4,399 Views
20 Pages

Reliability of liquid rocket engines is strictly connected with the successful operation of cooling jackets, able to sustain the impressive operative conditions in terms of huge thermal and mechanical loads, generated in thrust chambers. Cryogenic fu...

  • Article
  • Open Access
17 Citations
5,408 Views
23 Pages

Numerical and Experimental Investigation of Longitudinal Oscillations in Hall Thrusters

  • Vittorio Giannetti,
  • Manuel Martín Saravia,
  • Luca Leporini,
  • Simone Camarri and
  • Tommaso Andreussi

One of the main oscillatory modes found ubiquitously in Hall thrusters is the so-called breathing mode. This is recognized as a relatively low-frequency (10–30 kHz), longitudinal oscillation of the discharge current and plasma parameters. In this pap...

  • Article
  • Open Access
20 Citations
9,343 Views
24 Pages

Innovative Mechanical Design Strategy for Actualizing 80 kg-Class X-Band Active SAR Small Satellite of S-STEP

  • Seong-Cheol Kwon,
  • Ji-Hae Son,
  • Sung-Chan Song,
  • Jin-Han Park,
  • Kyung-Rae Koo and
  • Hyun-Ung Oh

The Small SAR Technology Experimental Project (S-STEP) mission aims to develop a new (space-based 80 kg-class active X-band synthetic aperture radar (SAR)) satellite with a main imaging mode of 1 m resolution stripmap. In the S-STEP mission, to achie...

  • Article
  • Open Access
13 Citations
9,030 Views
24 Pages

The CANYVAL-C (CubeSat Astronomy by NASA and Yonsei using a virtual telescope alignment for coronagraph) is a space science demonstration mission that involves taking several images of the solar corona with two CubeSats—1U CubeSat (Timon) and 2U Cube...

  • Article
  • Open Access
28 Citations
6,700 Views
24 Pages

Monte Carlo Predictions of Aero-Engine Performance Degradation Due to Particle Ingestion

  • Matthew Ellis,
  • Nicholas Bojdo,
  • Antonio Filippone and
  • Rory Clarkson

Aero-engines, which encounter clouds of airborne particulate, experience reduced performance due to the deposition of particles on their high-pressure turbine nozzle guide vanes. The rate of this degradation depends on particle properties, engine ope...

  • Article
  • Open Access
6 Citations
3,595 Views
17 Pages

Film cooling effectiveness can be improved significantly by embedding a round hole in trenches or craters. In this study, film cooling performances of a transverse trench, W-shaped trench and elliptic trench were compared and analyzed in detail. The...

  • Article
  • Open Access
3 Citations
5,966 Views
18 Pages

Engineering Comprehensive Model of Complex Wind Fields for Flight Simulation

  • Jianwei Chen,
  • Liangming Wang,
  • Jian Fu and
  • Zhiwei Yang

A complex wind field refers to the typical atmospheric disturbance phenomena existing in nature that have a great influence on the flight of aircrafts. Aimed at the issues involving large volume of data, complex computations and a single model in the...

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Aerospace - ISSN 2226-4310