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Aerospace, Volume 11, Issue 1

2024 January - 101 articles

Cover Story: A chemical reactor network model is proposed to simulate aeroengine burner emission and efficiency performance. In contrast to similar methods, its simplified partitioning into three subvolumes according to the axial distribution of the different air streams, paired with a proposed empirical tuning method, promotes the generality of the model without requiring engine-specific data. Its configuration produces a robust model capable of employing detailed kerosene combustion schemes to compute design-sensitive predictions of NOx, CO and unburnt hydrocarbons emissions. The model’s prediction trends are validated over actual engine tests and correlation methods, and it is integrated into open and closed design optimization loops to enhance the combustor’s performance. View this paper
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Articles (101)

  • Article
  • Open Access
6 Citations
5,076 Views
24 Pages

22 January 2024

Early and rapid environmental assessment of newly developed aircraft concepts is eminent in today’s climate debate. This can shorten the decision-making process and thus accelerate the entry into service of climate-friendly technologies. A holi...

  • Article
  • Open Access
1 Citations
2,987 Views
26 Pages

22 January 2024

In this study, we consider the problem of motion planning for urban air mobility applications to generate a minimal snap trajectory and trajectory that cost minimal time to reach a goal location in the presence of dynamic geo-fences and uncertainties...

  • Article
  • Open Access
4 Citations
2,021 Views
14 Pages

22 January 2024

A two-point cylindrical-focused laser differential interferometer (2P-CFLDI) system and a conventional Z-type Schlieren were used to measure the hypersonic turbulent boundary layer on a flat plate at Mach number Ma = 6 and Reynolds number Re = 1.08 &...

  • Article
  • Open Access
2 Citations
5,202 Views
17 Pages

Multi-Modal Life Cycle Assessment of Journeys by Aircraft, Train or Passenger Car

  • R. J. Roosien,
  • M. N. A. Lim,
  • S. M. Petermeijer and
  • W. F. Lammen

20 January 2024

To reduce the carbon footprint of transport, policymakers are simultaneously stimulating cleaner vehicles and more sustainable mobility choices, such as a shift to rail for short-haul flights within Europe. The purpose of this study is to determine t...

  • Article
  • Open Access
2 Citations
2,024 Views
16 Pages

20 January 2024

The unsteady combustion of solid propellants under oscillating environments is the key to understanding the combustion instability inside solid rocket motors. The discontinuous Galerkin–finite element method (DG-FEM) is introduced to provide an...

  • Article
  • Open Access
5 Citations
5,187 Views
20 Pages

A Deep Learning Approach for Trajectory Control of Tilt-Rotor UAV

  • Javensius Sembiring,
  • Rianto Adhy Sasongko,
  • Eduardo I. Bastian,
  • Bayu Aji Raditya and
  • Rayhan Ekananto Limansubroto

19 January 2024

This paper investigates the development of a deep learning-based flight control model for a tilt-rotor unmanned aerial vehicle, focusing on altitude, speed, and roll hold systems. Training data is gathered from the X-Plane flight simulator, employing...

  • Article
  • Open Access
4 Citations
2,738 Views
19 Pages

Development of a Novel Small-Scale Gust Generator Research Facility

  • Zhenlong Wu,
  • Tianyu Zhang,
  • Yuan Gao and
  • Huijun Tan

19 January 2024

In this paper, a novel small-scale gust generator research facility was designed and examined for generating Sears-type gusts. The design scheme, integration with the wind tunnel, experiment and validation of its capability are presented in detail. T...

  • Article
  • Open Access
3 Citations
2,984 Views
21 Pages

Large-Eddy Simulations of a Hypersonic Re-Entry Capsule Coupled with the Supersonic Disk-Gap-Band Parachute

  • Lakshmi Narayana Phaneendra Peri,
  • Antonella Ingenito and
  • Paolo Teofilatto

19 January 2024

The goal of this paper is to investigate the aerodynamic and aerothermodynamic behavior of the Schiaparelli capsule after the deployment of a supersonic disk-gap-band (DGB) parachute during its re-entry phase into the Martian atmosphere. The novelty...

  • Article
  • Open Access
3 Citations
2,089 Views
21 Pages

Flow Structure behind Spanwise Pin Array in Supersonic Flow

  • Philip A. Lax,
  • Skye Elliott,
  • Stanislav Gordeyev,
  • Matthew R. Kemnetz and
  • Sergey B. Leonov

19 January 2024

This work focused on the experimental characterization of a complex flow structure behind a cross-flow array of cylindrical pins installed on the wall of a supersonic duct. This geometry simulates several common gas dynamic configurations, such as a...

  • Review
  • Open Access
12 Citations
6,263 Views
55 Pages

18 January 2024

Maintenance strategies play a crucial role in ensuring the reliability and performance of complex systems. Imperfect inspections, characterized by the probabilities of false positives and false negatives, significantly impact the effectiveness of mai...

  • Article
  • Open Access
2 Citations
2,880 Views
20 Pages

18 January 2024

To achieve the commercialization of electric vertical takeoff and landing (eVTOL) aircrafts, which have recently garnered attention as the next-generation means of transportation, objective certification based on rigorous procedures is essential. Wit...

  • Article
  • Open Access
18 Citations
2,684 Views
22 Pages

18 January 2024

Bionic herringbone riblets are applied to relieve the flow near the blade endwall in a linear compressor cascade under the incidence angle of −4° to 6° at a Reynolds number of 382,000. The herringbone riblets are placed at the endwall u...

  • Article
  • Open Access
3 Citations
2,501 Views
20 Pages

18 January 2024

A special feature of airbreathing hypersonic aircraft is the complex coupling between aerodynamic and propulsive performances. This study presents a rapid analysis methodology for the integration of these two critical aspects in the conceptual design...

  • Article
  • Open Access
2,909 Views
22 Pages

Deciding Technosignature Search Strategies: Multi-Criteria Fuzzy Logic to Find Extraterrestrial Intelligence

  • Juan Miguel Sánchez-Lozano,
  • Eloy Peña-Asensio and
  • Hector Socas-Navarro

18 January 2024

This study presents the implementation of Multi-Criteria Decision-Making (MCDM) methodologies, particularly the fuzzy technique for order of preference by similarity to ideal solution (TOPSIS), in prioritizing technosignatures (TSs) for the search fo...

  • Article
  • Open Access
7 Citations
3,108 Views
29 Pages

18 January 2024

To find a trajectory with low radar detection probability for stealth aircraft under the assumption of 2D space, performing a rapid turning maneuver is a useful way to reduce the radar detection probability of an aircraft by changing the azimuth angl...

  • Article
  • Open Access
23 Citations
5,351 Views
20 Pages

Sustainability-Driven Design of Aircraft Composite Components

  • Angelos Filippatos,
  • Dionysios Markatos,
  • Georgios Tzortzinis,
  • Kaushik Abhyankar,
  • Sonia Malefaki,
  • Maik Gude and
  • Spiros Pantelakis

18 January 2024

The current prevailing trend in design across key sectors prioritizes eco-design, emphasizing considerations of environmental aspects in the design process. The present work aims to take a significant leap forward by proposing a design process where...

  • Article
  • Open Access
14 Citations
8,860 Views
21 Pages

Numerical Simulation of Heat Pipe Thermal Performance for Aerospace Cooling System Applications

  • Roberto Scigliano,
  • Valeria De Simone,
  • Roberta Fusaro,
  • Davide Ferretto and
  • Nicole Viola

17 January 2024

The design of integrated and highly efficient solutions for thermal management is a key capability for different aerospace products, ranging from civil aircraft using hydrogen on board to miniaturized satellites. In particular, this paper discloses a...

  • Article
  • Open Access
4,962 Views
19 Pages

A Solar Thermal Steam Propulsion System Using Disassociated Steam for Interplanetary Exploration

  • Leonard Vance,
  • Agustin Espinoza,
  • Jorge Martinez Dominguez,
  • Salil Rabade,
  • Gavin Liu and
  • Jekan Thangavelautham

17 January 2024

Sustainable space exploration will require using off-world resources for propellant generation. Using off-world-generated propellants significantly increases future missions’ range and payload capacity. Near Earth Objects (NEOs) contain a range...

  • Article
  • Open Access
16 Citations
6,108 Views
18 Pages

Mixed-Integer Linear Programming Model for Scheduling Missions and Communications of Multiple Satellites

  • Minkeon Lee,
  • Seunghyeon Yu,
  • Kybeom Kwon,
  • Myungshin Lee,
  • Junghyun Lee and
  • Heungseob Kim

16 January 2024

Satellites have been developed and operated for various purposes. The global satellite market is growing rapidly as the number of satellites and their mission diversity increase. Satellites revolve around the Earth to perform missions and communicate...

  • Article
  • Open Access
5 Citations
2,627 Views
21 Pages

16 January 2024

Unmanned aerial vehicle technology is the most advanced and helpful in almost every area of interest in human work. These devices become autonomous and can fulfil a variety of tasks, from simple imaging and obtaining data to search and rescue operati...

  • Article
  • Open Access
9 Citations
3,708 Views
12 Pages

Enhancing RDX Thermal Decomposition in Al@RDX Composites with Co Transition Metal Interfacial Layer

  • Su-Lan Yang,
  • Kan Xie,
  • Jing Wang,
  • Bingchen An,
  • Bin Tian,
  • Hongqi Nie,
  • Jie-Yao Lyu and
  • Qi-Long Yan

16 January 2024

In this study, an Al/Co@RDX composite was meticulously prepared through a combination of planetary high-energy ball-milling and a spray-drying technique. The thermal reactivity of these Al/Co@RDX composites was comprehensively investigated and compar...

  • Article
  • Open Access
4 Citations
2,567 Views
29 Pages

16 January 2024

The wing aerodynamic shape optimization is a typical high-dimensional problem with numerous independent design variables. Researching methods to reduce the dimensionality of optimization from the perspective of aerodynamic characteristics is necessar...

  • Article
  • Open Access
4 Citations
4,356 Views
53 Pages

15 January 2024

Research and industrial application can require custom high-level controllers for industrial drones. Thus, this paper presents the high-fidelity dynamic and control model identification of the DJI M600 Pro hexacopter. This is a widely used multicopte...

  • Article
  • Open Access
1 Citations
2,384 Views
18 Pages

15 January 2024

Tiltrotors permit aircrafts to operate vertically with lift, yet convert to ordinary forward flight with thrust. The challenge is to design a tiltrotor blade yielding maximum lift and thrust that converts smoothly without losing integrity or efficien...

  • Article
  • Open Access
4 Citations
2,944 Views
14 Pages

15 January 2024

Extensive research in predicting annual passenger throughput has been conducted, aiming at providing decision support for airport construction, aircraft procurement, resource management, flight scheduling, etc. However, how airport operational throug...

  • Article
  • Open Access
4 Citations
2,555 Views
18 Pages

Flow Characteristics of Liquid Jet in Transverse Shear Crossflow

  • Chi Zhang,
  • Yaguo Lyu,
  • Le Jiang and
  • Zhenxia Liu

13 January 2024

The numerical simulation method was used to investigate the deflection and deformation process of a circular lubricating oil jet in transverse shear airflow. The numerical model was compared and validated against the experimental data. The physical p...

  • Article
  • Open Access
11 Citations
10,145 Views
51 Pages

12 January 2024

High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow instability known as ‘buzz’, characterized by unsteady shock oscillations at the inlet. This paper presents a comprehensive review of prior researc...

  • Article
  • Open Access
6 Citations
2,771 Views
16 Pages

Autonomous Shape Decision Making of Morphing Aircraft with Improved Reinforcement Learning

  • Weilai Jiang,
  • Chenghong Zheng,
  • Delong Hou,
  • Kangsheng Wu and
  • Yaonan Wang

12 January 2024

The autonomous shape decision-making problem of a morphing aircraft (MA) with a variable wingspan and sweep angle is studied in this paper. Considering the continuity of state space and action space, a more practical autonomous decision-making algori...

  • Article
  • Open Access
7 Citations
3,548 Views
16 Pages

Enhancing Planetary Exploration through Digital Twins: A Tool for Virtual Prototyping and HUMS Design

  • Lucio Pinello,
  • Lorenzo Brancato,
  • Marco Giglio,
  • Francesco Cadini and
  • Giuseppe Francesco De Luca

12 January 2024

In recent times, the demand for resilient space rovers has surged, which has been driven by the amplified exploration of celestial bodies such as the Moon and Mars. Recognising the limitations of direct human intervention in such environments, these...

  • Article
  • Open Access
1 Citations
2,323 Views
21 Pages

12 January 2024

The effect of mixing on coupled heat release and transfer performance of a novel segregated solid motor is numerically evaluated with a transient two-dimensional combustion model. The results show that vortex structures are formed and evolved in the...

  • Article
  • Open Access
4 Citations
3,105 Views
16 Pages

Switching Logic for a Direct Hybrid Electric Powertrain

  • Robin Fonk,
  • Tobias Graf,
  • Sven Paeßler,
  • Christiane Bauer,
  • Josef Kallo and
  • Caroline Willich

12 January 2024

Hybrid electric aircraft with a powertrain based on fuel cells and batteries can reduce climate-active emissions in aviation. In a direct hybrid powertrain, the fuel cell and the battery are connected in parallel, without a DC/DC converter balancing...

  • Article
  • Open Access
5 Citations
3,111 Views
26 Pages

Aircraft Upset Recovery Strategy and Pilot Assistance System Based on Reinforcement Learning

  • Jin Wang,
  • Peng Zhao,
  • Zhe Zhang,
  • Ting Yue,
  • Hailiang Liu and
  • Lixin Wang

11 January 2024

The upset state is an unexpected flight state, which is characterized by an unintentional deviation from normal operating parameters. It is difficult for the pilot to recover the aircraft from the upset state accurately and quickly. In this paper, an...

  • Article
  • Open Access
1 Citations
5,148 Views
14 Pages

Design and Validation of a Photoelectric Current Measuring Unit for Lunar Daytime Simulation Chamber

  • Seungsoo Park,
  • Taeil Chung,
  • Jihyun Kim,
  • Byunghyun Ryu and
  • Hyusoung Shin

11 January 2024

Charging of the lunar surface induced by solar radiation can potentially threaten in situ resource utilization. Associated issues include dust adhesion and material degradation. Photoelectric currents are the primary cause of surface charging. This w...

  • Article
  • Open Access
10 Citations
3,212 Views
35 Pages

10 January 2024

Airworthiness certification requires proof of structure strength, which is performed generally through a building block approach. To achieve this, representative intermediate-scale experiments generated by test benches are, in general, needed, in add...

  • Article
  • Open Access
5 Citations
2,509 Views
19 Pages

10 January 2024

The use of film cooling technology is one of the most effective ways to minimize the damage to wall materials caused by the high-temperature environment in a ramjet. Optimization of the design to achieve the highest film cooling efficiency on the hot...

  • Article
  • Open Access
3 Citations
3,392 Views
23 Pages

Parameter Tuning of a Vapor Cycle System for a Surveillance Aircraft

  • Adelia Darlene Drego,
  • Daniel Andersson and
  • Ingo Staack

10 January 2024

Surveillance aircraft perform long-duration missions (>eight hours) that include detection and identification of objects on the ground, the water, or in the air. They have surveillance systems that require large amounts of cooling power (typically...

  • Article
  • Open Access
2 Citations
1,762 Views
15 Pages

10 January 2024

The spaceborne solar observation system is crucial for the study of space phenomena such as solar flares, which requires high tracking accuracy. This study presents a coupling model that integrates mechanical, electrical, and control models to invest...

  • Article
  • Open Access
2 Citations
2,485 Views
21 Pages

Busemann’s supersonic biplane airfoil can reduce wave drag through shock interactions at its designed freestream Mach number. However, a choking phenomenon occurs with a decrease in the freestream Mach number, and the drag coefficient increases...

  • Article
  • Open Access
1 Citations
3,572 Views
11 Pages

Study of Starting Performance of a Series Hybrid Aero Propulsion System

  • Jianfeng Zhu,
  • Guochen Huang,
  • Maoguang Xu,
  • Ming Liu,
  • Bo Diao and
  • Po Li

Combined with the development trend of high speed generators and the high voltage of DC microgrids in high-power series hybrid aero propulsion system, a set of hybrid systems with a power of 200 kW, voltage of 540 V, and speed of 21,000 r/min is esta...

  • Article
  • Open Access
3 Citations
2,566 Views
16 Pages

Robust Flight Tether for In-Orbit Demonstrations of Coulomb Drag Propulsion

  • Petri Toivanen,
  • Pekka Janhunen,
  • Jarmo Kivekäs and
  • Meri Mäkelä

A new method of producing robust multi-wire tethers for Coulomb drag applications was developed. The multi-wire structure required for redundancy against the micrometeoroid flux of the space environment is realised through the method of wire twist bo...

  • Article
  • Open Access
2 Citations
2,699 Views
24 Pages

Design and Machining of a Spherical Shell Rotor for a Magnetically Levitated Momentum Ball

  • Limei Ma,
  • Yongheng Zhang,
  • Yuli Niu,
  • Yong Zhao,
  • Shaoya Guan,
  • Zijing Wang and
  • Tuoda Wu

Ball-shell rotors with non-standard shapes, non-uniform conductive coatings, and eccentric masses machined by conventional processes constrain the improvement of levitation and torque accuracy of magnetically levitated momentum balls. This paper focu...

  • Article
  • Open Access
7 Citations
3,288 Views
14 Pages

Experimental Study on Hypersonic Double-Wedge Induced Flow Based on Plasma Active Actuation Array

  • Bo Yang,
  • Hesen Yang,
  • Ning Zhao,
  • Hua Liang,
  • Zhi Su and
  • Dongsheng Zhang

The double-wedge configuration is a typical characteristic shape of the rudder surface of high-speed aircraft. The impact of the shock wave/boundary layer interaction and the shock wave/shock wave interaction resulting from the double wedge on aircra...

  • Article
  • Open Access
2 Citations
2,267 Views
17 Pages

This paper investigates the performance of the forthcoming lunar navigation satellite systems for estimating not only the position of an onboard receiver in a lunar inertial reference frame but also, and with a consistent accuracy, the relative posit...

  • Article
  • Open Access
4 Citations
2,559 Views
16 Pages

Temperatures within the boundary layers of high-enthalpy hypersonic flows can soar to thousands or even tens of thousands of degrees, leading to significant real gas phenomena. Although there has been significant research on real gas effects on hyper...

  • Article
  • Open Access
2 Citations
2,353 Views
14 Pages

A Neural Network-Based Flame Structure Feature Extraction Method for the Lean Blowout Recognition

  • Puti Yan,
  • Zhen Cao,
  • Jiangbo Peng,
  • Chaobo Yang,
  • Xin Yu,
  • Penghua Qiu,
  • Shanchun Zhang,
  • Minghong Han,
  • Wenbei Liu and
  • Zuo Jiang

A flame’s structural feature is a crucial parameter required to comprehensively understand the interaction between turbulence and flames. The generation and evolution processes of the structure feature have rarely been investigated in lean blow...

  • Article
  • Open Access
3 Citations
1,810 Views
20 Pages

Design of Convergent and Accurate Guidance Law with Finite Time in Complex Adversarial Scenarios

  • Hang Ding,
  • Dongdong Wang,
  • Chuanjun Li,
  • Xiao Liang and
  • Xingcheng Li

The target can deceive the flight vehicle by releasing an infrared decoy to make the line-of-sight (LOS) angle rate deflect greatly, thus causing the flight vehicle to miss the target. Therefore, in order to accurately strike the target in complex ad...

  • Article
  • Open Access
3 Citations
2,509 Views
26 Pages

The concept of the Fan Wing, a novel aircraft vector-force-integrated device that combines a power unit with a fixed wing to generate distributed lift and thrust by creating a low-pressure vortex on the wing’s surface, was studied. To investiga...

  • Article
  • Open Access
6 Citations
2,283 Views
20 Pages

Due to its advantages of easy deployment and high stiffness-to-mass ratio, the utilization of truss structures for constructing large satellites presents an appealing solution for modern space missions, including Earth observation and astronomy. Howe...

  • Article
  • Open Access
3 Citations
2,903 Views
30 Pages

This study examines the wing hinge oscillations in an aircraft concept that employs multiple wings, or small aircraft, chained at the wing tips through freely rotatable hinges with minimal structural damping and no mechanical position-locking system....

  • Article
  • Open Access
5 Citations
3,071 Views
19 Pages

A Study for a Radio Telescope in Indonesia: Parabolic Design, Simulation of a Horn Antenna, and Radio Frequency Survey in Frequency of 0.045–18 GHz

  • Peberlin Parulian Sitompul,
  • Pakhrur Razi,
  • Timbul Manik,
  • Mario Batubara,
  • Musthofa Lathif,
  • Farahhati Mumtahana,
  • Rizal Suryana,
  • Ibnu Nurul Huda,
  • Taufiq Hidayat and
  • Farhan Sobirin
  • + 1 author

After years of preparation, the Indonesia National Observatory, located in Mount Timau, Kupang Regency, is currently in the completion stage of research in astronomy and astrophysics and related subjects. An optic telescope with a 3.8 m diameter is e...

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Aerospace - ISSN 2226-4310