Skip to Content
You are currently on the new version of our website. Access the old version .

Aerospace, Volume 11, Issue 7

2024 July - 100 articles

Cover Story: Space launch and satellite propulsion engineers strive for every little improvement in system performance to increase payload capacity. Aerospike nozzles, with their altitude-adaptive characteristics, can provide such an additional performance gain in comparison with conventional bell nozzles. A key aspect for the successful implementation of this advanced nozzle concept is thrust vector control (TVC). This paper provides insights into the impact of aerodynamic TVC on the nozzle surface and base pressure distribution of a linear aerospike through secondary injection. The results presented are obtained via cold-gas experiments on a linear aerospike nozzle, providing a reference and starting point for further numerical and experimental analyses. View this paper
  • Issues are regarded as officially published after their release is announced to the table of contents alert mailing list .
  • You may sign up for email alerts to receive table of contents of newly released issues.
  • PDF is the official format for papers published in both, html and pdf forms. To view the papers in pdf format, click on the "PDF Full-text" link, and use the free Adobe Reader to open them.

Articles (100)

  • Article
  • Open Access
1 Citations
2,997 Views
15 Pages

Parasitic SAR formation can be flown at low altitude using smaller satellites and adding potential to conventional SAR mission From the orbital point of view, the main issue is related to the differential aerodynamic drag, which rapidly disrupts the...

  • Article
  • Open Access
4 Citations
3,924 Views
19 Pages

ATC-SD Net: Radiotelephone Communications Speaker Diarization Network

  • Weijun Pan,
  • Yidi Wang,
  • Yumei Zhang and
  • Boyuan Han

This study addresses the challenges that high-noise environments and complex multi-speaker scenarios present in civil aviation radio communications. A novel radiotelephone communications speaker diffraction network is developed specifically for these...

(This article belongs to the Special Issue Advances in Air Traffic and Airspace Control and Management (2nd Edition))
  • Article
  • Open Access
4 Citations
3,354 Views
14 Pages

Safe and Efficient Exploration Path Planning for Unmanned Aerial Vehicle in Forest Environments

  • Youkyung Hong,
  • Suseong Kim,
  • Youngsun Kwon,
  • Sanghyouk Choi and
  • Jihun Cha

This study presents an enhanced exploration path planning for unmanned aerial vehicles. The primary goal is to increase the chances of survival of missing people in forest environments. Exploration path planning is an essential methodology for explor...

  • Article
  • Open Access
2 Citations
2,288 Views
19 Pages

Integrated Waverider Forebody/Inlet Fusion Method Based on Discrete Point Cloud Reconstruction

  • Zhiqi Liu,
  • Geling Yin,
  • Mingqiang Luo,
  • Jinrong Zhang and
  • Cheekeat Heng

The integrated design of waverider forebodies and inlets is considered a critical challenge in high Mach number vehicle development. To facilitate the rapid construction of integrated geometrical models for waverider forebodies and inlets during the...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
10 Citations
2,892 Views
14 Pages

The safety of airport runways is important to guarantee aircraft taking-off, landing, and taxiing, and the comparison of the mechanical response of pavement structures under dynamic and static loading by LS-DYNA has rarely been studied. The purpose o...

  • Article
  • Open Access
6 Citations
2,392 Views
28 Pages

This paper presents models for UAV aerial-towed cables in free-end and fixed-end configurations, crucial for tasks like communication and aerial charging. By establishing a quasi steady-state model, computational results on cable shapes are obtained....

(This article belongs to the Special Issue Aerodynamic and Multidisciplinary Design Optimization)
  • Article
  • Open Access
5 Citations
2,775 Views
24 Pages

Experimental Study of the Aerodynamic Performance and Flow Characteristics of an Integrated UAV Inlet with Double 90° Bends

  • Jiahao Ren,
  • Zhenlong Wu,
  • Huijun Tan,
  • Ziyun Wang and ,
  • Xiaoming He,
  • Dongpo Li and
  • Yi Zhou
  • + 2 authors+ 0 author

Many UAVs today have an S-bend inlet for the sake of stealth; however, the majority of them have a relatively gentle transition of the flow channel. This study presents an experimental investigation of the aerodynamic performance and swirl flow chara...

  • Article
  • Open Access
3 Citations
2,233 Views
23 Pages

Analysis of the Effect of Sampling Probe Geometry on Measurement Accuracy in Supersonic Gas Flow

  • Wanlin Zhang,
  • Yingtao Chen,
  • Yanting Ai,
  • Pengpeng Sha and
  • Xinlong Yang

The accuracy of sampling of gas components has a significant impact on the measurement of various performance parameters in the combustion chamber of an aero-engine. In order to investigate the effect of the probe geometry of a six-point gas sampling...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
5 Citations
3,539 Views
19 Pages

On the Generalization Capability of a Data-Driven Turbulence Model by Field Inversion and Machine Learning

  • Yasunari Nishi,
  • Andreas Krumbein,
  • Tobias Knopp,
  • Axel Probst and
  • Cornelia Grabe

This paper discusses the generalizability of a data-augmented turbulence model with a focus on the field inversion and machine learning approach. It is highlighted that the augmented model based on two-dimensional (2D) separated airfoil flows gives p...

(This article belongs to the Special Issue Data-Driven Aerodynamic Modeling)
  • Article
  • Open Access
2 Citations
1,961 Views
15 Pages

The accumulation of ice on the aero-engine inlet compromises engine safety. Traditional hot air anti-icing systems, which utilize bleed air, require substantial energy, decreasing engine performance and increasing emissions. Superhydrophobic material...

(This article belongs to the Special Issue Deicing and Anti-Icing of Aircraft (Volume III))
  • Article
  • Open Access
20 Citations
4,246 Views
26 Pages

Preliminary Sizing of High-Altitude Airships Featuring Atmospheric Ionic Thrusters: An Initial Feasibility Assessment

  • Carlo E.D. Riboldi,
  • Marco Belan,
  • Stefano Cacciola,
  • Raffaello Terenzi and ,
  • Stefano Trovato,
  • Davide Usuelli and
  • Giuseppe Familiari
  • + 2 authors+ 0 author

When it comes to computing the values of variables defining the preliminary sizing of an airship, a few standardized approaches are available in the existing literature. However, when including a disruptive technology in the design is required, sizin...

(This article belongs to the Special Issue Mission Analysis and Design of Lighter-than-Air Flying Vehicles (2nd Edition))
  • Article
  • Open Access
8 Citations
3,770 Views
24 Pages

New Data-Driven Models of Mass Flow Rate and Isentropic Efficiency of Dynamic Compressors

  • Xiande Fang,
  • Yuxiang Fang,
  • Yang Yang,
  • Zhiqiang He and
  • Bei Yang

Dynamic compressors are widely used in many industrial sectors, such as air, land, and marine vehicle engines, aircraft environmental control systems (ECS), air-conditioning and refrigeration, gas turbines, gas compression and injection, etc. The dat...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
9 Citations
3,057 Views
21 Pages

Hybrid Detection Method for Multi-Intent Recognition in Air–Ground Communication Text

  • Weijun Pan,
  • Zixuan Wang,
  • Zhuang Wang,
  • Yidi Wang and
  • Yuanjing Huang

In recent years, the civil aviation industry has actively promoted the automation and intelligence of control processes with the increasing use of various artificial intelligence technologies. Air–ground communication, as the primary means of i...

  • Article
  • Open Access
1 Citations
2,855 Views
13 Pages

Contrails are estimated to contribute 2% of the Earth’s anthropogenic global warming. Contrails are ice crystal clouds formed by the emission of soot and water vapor from jet engines in atmospheric conditions known as Ice Super Saturated (ISS)...

(This article belongs to the Special Issue Advances in Air Traffic and Airspace Control and Management (2nd Edition))
  • Article
  • Open Access
8 Citations
5,885 Views
31 Pages

Airfoil Design Optimization of Blended Wing Body for Various Aerodynamic and Stealth Stations

  • Wei Zhang,
  • Lin Zhou,
  • Ke Zhao,
  • Ruibin Zhang and ,
  • Zhenghong Gao and
  • Bowen Shu
  • + 1 author+ 0 author

The airfoil is the foundation of an aircraft, and its characteristics have a significant impact on those of the aircraft. Conventional airfoil design mainly focuses on improving aerodynamic performance, while flying wing airfoil designs should also c...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
16 Citations
6,917 Views
31 Pages

Cooling of 1 MW Electric Motors through Submerged Oil Impinging Jets for Aeronautical Applications

  • Giuseppe Di Lorenzo,
  • Diego Giuseppe Romano,
  • Antonio Carozza and
  • Antonio Pagano

Electrification of aircraft is a very challenging task as the demand for energy and power is high. While the storage and generation of electrical energy are widely studied due to the limited specific energy and specific power of batteries and fuel ce...

(This article belongs to the Special Issue Electric Machines for Electrified Aircraft Propulsion)
  • Article
  • Open Access
15 Citations
4,908 Views
17 Pages

Urban air mobility is an effective solution to address the current issue of ground traffic congestion in future cities. However, as the user scale continues to expand, the current civil aviation flight scheduling and control methods are becoming inad...

(This article belongs to the Section Air Traffic and Transportation)
  • Article
  • Open Access
3 Citations
2,415 Views
24 Pages

A Time-Domain Calculation Method for Gust Aerodynamics in Flight Simulation

  • Zexuan Yang,
  • Chao Yang,
  • Daxin Wen,
  • Wenbo Zhou and
  • Zhigang Wu

Gusts have a significant impact on aircraft and need to be analyzed through flight simulations. The solution for time-domain gust aerodynamic forces stands as a pivotal stage in this process. With the increasing demand for flight simulations within g...

(This article belongs to the Special Issue Gust Influences on Aerospace)
  • Article
  • Open Access
9 Citations
3,321 Views
28 Pages

Architecture Preliminary Design and Trade-Off Optimization of Stratospheric Airship Based on MBSE

  • Weihao Lyu,
  • Yanchu Yang,
  • Jinggang Miao,
  • Shenghong Cao and
  • Lingsen Kong

System architecture design is crucial for forward design in aerostat system engineering, yet a comprehensive research framework has been lacking. This paper presents a new method for stratospheric airship architecture preliminary design and optimizat...

(This article belongs to the Special Issue Mission Analysis and Design of Lighter-than-Air Flying Vehicles (2nd Edition))
  • Article
  • Open Access
3,325 Views
18 Pages

The quality of air traffic control speech is crucial. However, internal and external noise can impact air traffic control speech quality. Clear speech instructions and feedback help optimize flight processes and responses to emergencies. The traditio...

(This article belongs to the Special Issue Advances in Air Traffic and Airspace Control and Management (2nd Edition))
  • Article
  • Open Access
8 Citations
2,654 Views
23 Pages

A rapid trajectory-planning method based on an analytical predictor–corrector design of drag acceleration profile and a bank-reversal logic based on double-stage adaptive adjustment is proposed to solve the entry issue under time and full-state...

(This article belongs to the Special Issue Dynamics, Guidance and Control of Aerospace Vehicles)
  • Article
  • Open Access
3 Citations
4,216 Views
13 Pages

Experimental Determination of Pitch Damping Coefficient Using Free Oscillation Method

  • Ionuț Bunescu,
  • Mihăiță-Gilbert Stoican and
  • Mihai-Vlăduț Hothazie

This paper outlines an experimental investigation conducted at the INCAS trisonic wind tunnel, focusing on the determination of pitch damping coefficient. The model used for this investigation is the Basic Finner Model, a standard model for dynamic t...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1 Citations
2,643 Views
29 Pages

Ground-Based Characterisation of a Compact Instrument for Gamma-ray Burst Detection on a CubeSat Platform

  • Rachel Dunwoody,
  • David Murphy,
  • Alexey Uliyanov,
  • Joseph Mangan and ,
  • Maeve Doyle,
  • Joseph Thompson,
  • Cuan de Barra,
  • Lorraine Hanlon,
  • David McKeown and
  • Sheila McBreen
  • + 6 authors+ 1 author

Gamma-ray bursts (GRBs) are intense and short-lived cosmic explosions. Miniaturised CubeSat-compatible instruments for the study of GRBs are being developed to help bridge the gap in large missions and assist in achieving full sky coverage. CubeSats...

(This article belongs to the Special Issue Space Telescopes & Payloads)
  • Article
  • Open Access
1 Citations
1,983 Views
21 Pages

Design of Low-Cost Simulation Space Micro Debris Launch Device

  • Renjie Yang,
  • Kai Tang,
  • Xuqiang Lang,
  • Cheng He and ,
  • Yu Liu and
  • Yue Liu
  • + 1 author+ 0 author

The high cost and low emission frequency of microparticle launchers have resulted in a long lead time for the development of detectors for micro-debris in space. In this paper, two low-cost, high-emission-frequency, small-size, millimeter-sized parti...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
1 Citations
3,201 Views
15 Pages

Design and Implementation of a Land-Air Omnidirectional Mobile Robot

  • Changlong Ye,
  • Hongyu Wang,
  • Suyang Yu,
  • Xinyu Ma and
  • Ruizhe Zhou

This paper proposes a new type of omnidirectional mobile robot for land and air, which has three motion modes, combines the motion characteristics of land motion and air flight, has the ability to climb walls, and can be actively deformed to adapt to...

  • Review
  • Open Access
13 Citations
6,544 Views
23 Pages

As global warming intensifies, the world is increasingly concerned about carbon emissions. As an important industry that affects carbon emissions, the air transportation industry takes on the important task of energy saving and emission reduction. Fo...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
1,900 Views
23 Pages

A Novel Approach Using Non-Experts and Transformation Models to Predict the Performance of Experts in A/B Tests

  • Phillip Stranger,
  • Peter Judmaier,
  • Gernot Rottermanner,
  • Carl-Herbert Rokitansky and ,
  • Istvan-Szilard Szilagyi,
  • Volker Settgast and
  • Torsten Ullrich
  • + 2 authors+ 0 author

The European Union is committed to modernising and improving air traffic management systems to promote environmentally friendly air transport. However, the safety-critical nature of ATM systems requires rigorous user testing, which is hampered by the...

(This article belongs to the Special Issue Human Factors during Flight Operations)
  • Article
  • Open Access
2,070 Views
22 Pages

This study investigates the evaporation and ignition characteristics of a single droplet of ammonium dinitramide (ADN)-based liquid propellant utilizing a waveguide resonant cavity device, in conjunction with a high-speed photographic imaging system...

  • Article
  • Open Access
7 Citations
2,411 Views
26 Pages

Hypersonic vehicles are susceptible to considerable aerodynamic heating and noticeable aerothermoelastic effects during flight due to their high speeds. Functionally graded materials (FGMs), which enable continuous changes in material properties by v...

(This article belongs to the Special Issue Aeroelasticity, Volume IV)
  • Article
  • Open Access
1 Citations
2,114 Views
24 Pages

In this study, the aerodynamic performance of a cambered wind turbine airfoil with a partially flexible membrane material on its suction surface was examined experimentally across various angles of attack and Reynolds numbers. It encompassed physical...

  • Review
  • Open Access
12 Citations
17,229 Views
29 Pages

Rotating detonation engines (RDEs), which are Humphrey cycle-based constant-volume combustion engines, utilize detonation waves to attain higher efficiencies compared with conventional constant-pressure combustion engines through pressure gain. Such...

(This article belongs to the Special Issue Advances in Detonative Propulsion)
  • Article
  • Open Access
3 Citations
3,492 Views
23 Pages

Incidence Adaptation to the Influence of Wake Sweeps on the Aerodynamic Performance of a Low-Pressure Turbine Cascade

  • Xuejian Li,
  • Xinglong Fang,
  • Le Cai,
  • Lan Wang and ,
  • Xinlei Hu,
  • Yingjie Chen and
  • Songtao Wang
  • + 2 authors+ 0 author

In order to investigate the transport law of an unsteady wake in a downstream cascade channel in a turbine stage environment, this study was based on a self-designed unsteady wake generator, and a low-pressure turbine cascade was the research object....

  • Article
  • Open Access
5 Citations
2,665 Views
22 Pages

Evaluating the mission efficiency of various drone configurations under complex, multi-source, and multi-dimensional requirements remains a significant challenge. This study aimed to develop a comprehensive decision support system (DSS) that employs...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
6 Citations
2,119 Views
24 Pages

The design of a hypersonic vehicle controller has been an active research field in the last decade, especially when the vehicle is studied as a time-varying system. A time-varying compound control method is proposed for a hypersonic vehicle controlle...

(This article belongs to the Special Issue Challenges and Innovations in Aircraft Flight Control)
  • Article
  • Open Access
5 Citations
2,808 Views
20 Pages

Design of Entire-Flight Pinpoint Return Trajectory for Lunar DRO via Deep Neural Network

  • Xuxing Huang,
  • Baihui Ding,
  • Bin Yang,
  • Renyuan Xie and ,
  • Zhengyong Guo,
  • Jin Sha and
  • Shuang Li
  • + 2 authors+ 0 author

Lunar DRO pinpoint return is the final stage of manned deep space exploration via a lunar DRO station. A re-entry capsule suffers from complicated dynamic and thermal effects during an entire flight. The optimization of the lunar DRO return trajector...

(This article belongs to the Special Issue Deep Space Exploration)
  • Article
  • Open Access
2 Citations
2,421 Views
17 Pages

In the defense and security domain, scenarios are often descriptions of stakeholder needs, future events, and the environment. They are used for the elicitation of requirements in development of capabilities, organizations, and technical systems. In...

(This article belongs to the Section Aeronautics)
  • Review
  • Open Access
2 Citations
5,026 Views
13 Pages

Engine failure after take-off (or one engine being inoperative) is an exercise conducted as part of multi-engine flight training and on-going competency checking. To prepare pilots to manage a real in-flight emergency, this exercise has traditionally...

(This article belongs to the Special Issue Human Factors during Flight Operations)
  • Article
  • Open Access
6 Citations
5,200 Views
22 Pages

Orbital maneuver detection for non-cooperative targets in space is a key task in space situational awareness. This study develops a passive maneuver detection algorithm using line-of-sight angles measured by a space-based optical sensor, especially f...

(This article belongs to the Special Issue Spacecraft Dynamics and Control (2nd Edition))
  • Article
  • Open Access
7 Citations
6,995 Views
18 Pages

The Oh-Park methodology was proposed to overcome the limitations of Steinberg’s theory for evaluating the structural safety of space-borne electronics and has been experimentally verified at the printed circuit board (PCB) specimen level for va...

(This article belongs to the Special Issue Advanced Design for Lightweight Space Materials and Structural Systems)
  • Article
  • Open Access
13 Citations
7,024 Views
19 Pages

Aerodynamic/stealth optimization is a key issue during the design of a stealth UAV. Balancing the weight of different incident angles of the RCS and combining stealth characteristics with aerodynamic characteristics are hotspots of aerodynamic/stealt...

  • Article
  • Open Access
2,087 Views
11 Pages

Spitzer Resurrector Mission: Advantages for Space Weather Research and Operations

  • Shawn M. Usman,
  • Giovanni G. Fazio,
  • Christopher A. Grasso,
  • Ryan C. Hickox and ,
  • Cameo Lance,
  • William B. Rideout,
  • Daveanand M. Singh,
  • Howard A. Smith,
  • Angelos Vourlidas and
  • Salma Benitez
  • + 10 authors+ 5 authors

In 1979, NASA established the Great Observatory program, which included four telescopes (Hubble, Compton, Chandra, and Spitzer) to explore the Universe. The Spitzer Space Telescope was launched in 2003 into solar orbit, gradually drifting away from t...

(This article belongs to the Special Issue Space Telescopes & Payloads)
  • Article
  • Open Access
6 Citations
4,512 Views
20 Pages

A micro-pulse detonation engine (μPDE) was designed and installed to a direct-connect scramjet combustor of Pusan National University (PNU-DCSC). The active excitation on the scramjet combustor was experimentally studied using the μPDE operatin...

  • Article
  • Open Access
10 Citations
3,322 Views
22 Pages

To achieve the intelligent interception of different types of maneuvering evaders, based on deep reinforcement learning, a novel intelligent differential game guidance law is proposed in the continuous action domain. Different from traditional guidan...

(This article belongs to the Special Issue Dynamics, Guidance and Control of Aerospace Vehicles)
  • Article
  • Open Access
3 Citations
2,327 Views
20 Pages

Fly-around-the-World Near-Space Picosatellite for Cost-Effective School Space Projects

  • Pirada Techavijit,
  • Polkit Sukchalerm,
  • Natthapong Wongphuangfuthaworn and
  • Sureepon Kiyapaet

This research presents the design and development of a near-space picosatellite platform intended to operate at high altitudes between 20–40 km above sea level. These picosatellites function similarly to orbital satellites but float and travel...

(This article belongs to the Section Astronautics & Space Science)
  • Article
  • Open Access
6 Citations
3,038 Views
19 Pages

Compound Attitude Control Strategy for Reusable Launch Vehicle Based on Improved Particle Swarm Optimization Algorithm

  • Shunfu Yang,
  • Lu Gan,
  • Tianyi Wang,
  • Enze Zhu and ,
  • Ling Yang and
  • Hu Chen
  • + 1 author+ 0 author

This study introduces an advanced dual-mode compound attitude control framework for reusable launch vehicles (RLVs), underpinned by an enhanced particle swarm optimization (PSO) algorithm. This innovative strategy is tailored to meet the stringent de...

(This article belongs to the Section Aeronautics)
  • Article
  • Open Access
2 Citations
2,255 Views
24 Pages

Despite considerable research effort in the past 60 years, the occurrence of combustion instabilities in rocket engines is still not fully understood. While the physical mechanisms involved have been studied separately and are well understood in a co...

(This article belongs to the Special Issue Space Propulsion: Advances and Challenges (2nd Edition))
  • Article
  • Open Access
1 Citations
3,269 Views
18 Pages

Study on Heat Transfer Characteristics of Jet Impingement of Turbine Bending Surface

  • Fei Zeng,
  • Ruijia Sun,
  • Zhenhua Chen,
  • Yuang Liu and
  • Weihua Yang

The architecture of aeroengine air-cooling system channels is notably intricate, with impingement heat transfer standing out as a critical process amidst the complexity. This study delves into the casing annular cavity’s structure, examining th...

  • Article
  • Open Access
1 Citations
2,467 Views
20 Pages

Design of Reverse Bleed Slot for Curved Axisymmetric Inlet Based on Kantrowitz Criterion and Flow Field Characteristics

  • Yongzhou Li,
  • Di Sun,
  • Xinhui Tian,
  • Yiqi Yuan and ,
  • Xisheng Luo and
  • Kunyuan Zhang
  • + 1 author+ 0 author

Conventional forward bleed slots reduce the hypersonic inlet starting Mach number but suffer from excessive flow leakage after restart. This paper proposes a novel reverse bleed slot design method for curved axisymmetric inlets of a solid-fuel scramj...

(This article belongs to the Special Issue Combustion of Solid Propellants)
  • Article
  • Open Access
10 Citations
3,130 Views
19 Pages

Three-Dimensional Characterization of Residual Stress in Aircraft Riveted Panel Structures

  • Yonggang Kang,
  • Huan Xiao,
  • Zihao Wang,
  • Guomao Li and
  • Yonggang Chen

The residual stress field induced by interference-fit riveting in aircraft panel structures significantly affects the fatigue performance around the rivet holes. Common residual stress analytical models often overlook the non-uniformity of interferen...

  • Article
  • Open Access
8 Citations
2,880 Views
16 Pages

Inter-Satellite Link Prediction with Supervised Learning: An Application in Polar Orbits

  • Estel Ferrer,
  • Joan A. Ruiz-De-Azua,
  • Francesc Betorz and
  • Josep Escrig

Distributed space systems are increasingly valued in the space industry, as they enhance mission performance through collaborative efforts and resource sharing among multiple heterogeneous satellites. Additionally, enabling autonomous and real-time s...

(This article belongs to the Special Issue Advanced Technology of Distributed Space Systems: Formation-Flying, Swarms, and Constellations)

of 2

XFacebookLinkedIn
Aerospace - ISSN 2226-4310