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Space sails for achieving major space exploration goals: Historical review and future outlook Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-11-07 Maximilien Berthet, James Schalkwyk, Onur Çelik, Debdut Sengupta, Ken Fujino, Andreas M. Hein, Luciana Tenorio, Josué Cardoso dos Santos, S. Peter Worden, Philip D. Mauskopf, Yasuyuki Miyazaki, Ikkoh Funaki, Shinjiro Tsuji, Piotr Fil, Kojiro Suzuki
Space sails are a continuum of lightweight, thin, large-area, deployable technologies which are pushing forward new frontiers in space mobility and exploration. They encompass solar sails, laser-driven sails, drag sails, magnetic sails, electric sails, deployable membrane reflectors, deployable membrane antennas, and solar power sails. Some have been flight tested with operational heritage, while some
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A comprehensive review of lunar-based manufacturing and construction Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-11-02 Mohammad Azami, Zahra Kazemi, Sare Moazen, Martine Dubé, Marie-Josée Potvin, Krzysztof Skonieczny
As humankind prepares to establish outposts and infrastructure on the Moon, the ability to manufacture parts and buildings on-site is crucial. While transporting raw materials from Earth can be costly and time-consuming, in-situ resource utilization (ISRU) presents an attractive alternative. This review paper aims to provide a thorough examination of the current state and future potential of Lunar-based
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Compressible vortex loops and their interactions Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-11-01 Murugan Thangadurai, Konstantinos Kontis, Craig White, Abhishek Kundu
Vortex loops are compact toroidal structures wherein fluid rotation forms a closed loop around a fictitious axis, manifest in many natural occurrences. These phenomena result from brief impulses through vents or apertures in fluid systems, such as in caves, volcanic crusts, downbursts, or the descent of liquid droplets. The majority of naturally occurring and laboratory-generated vortex loops, studied
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Responsive tolerant control: An approach to extend adaptability of launch vehicles Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-07-29 Zhengyu Song, Hao Pan, Menghan Shao
This paper reviews the development and state-of-the-art research of attitude control technologies for launch vehicles, as well as the application evaluations of the responsive tolerant control (RTC) technology. First, the control theories and methods related to launch vehicles are classified and surveyed. Although studies in this field are still active, many new methods have not exhibited impressive
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A systematic review of design for additive manufacturing of aerospace lattice structures: Current trends and future directions Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-07-17 Numan Khan, Aniello Riccio
Lattice structures, produced by repeated unit cells in the particular pattern, offer a high strength-to-weight ratio. The current advancement in Additive manufacturing (AM) technology, creating complex geometries like lattice structures has revolutionized production across various industries. While several reviews have focused on different specific aspects of lattice structures, a comprehensive overview
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Prediction of concentrated vortex aerodynamics: Current CFD capability survey Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-07-06 James M. Luckring, Arthur Rizzi
Concentrated vortex flows contribute to the aerodynamic performance of aircraft at elevated load conditions. For military interests, the vortex flows are exploited at maneuver conditions of combat aircraft and missiles. For transport interests, the vortex flows are exploited at takeoff and landing conditions as well as at select transonic conditions. Aircraft applications of these vortex flows are
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A comprehensive review on Cislunar expansion and space domain awareness Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-07-05 Brian Baker-McEvilly, Surabhi Bhadauria, David Canales, Carolin Frueh
The Cislunar region is crucial for expanding human presence in space in the forthcoming decades. This paper presents a comprehensive review of recent and anticipated Earth–Moon missions, and ongoing space domain awareness initiatives. An introduction to the dynamics as well as periodic trajectories in the Cislunar realm is presented. Then, a review of modern Cislunar programs as well as smaller missions
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Enhancing detonation propulsion with jet in cross-flow: A comprehensive review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-06-25 Bo Zhang
Compared with traditional deflagration-based systems, detonation-based propulsion systems offer significant potential benefits in terms of efficiency and specific impulses in the field of advanced aerospace propulsion technologies. However, the successful implementation of these technologies faces several key challenges, particularly in achieving reliable, stable, and robust detonation wave propagation
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Friction damping for turbomachinery: A comprehensive review of modelling, design strategies, and testing capabilities Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-06-19 Jie Yuan, Chiara Gastaldi, Enora Denimal Goy, Benjamin Chouvion
This paper presents a comprehensive review of recent advancements in modelling approaches, design strategies, and testing techniques applied to friction damping in turbomachinery. It critically evaluates experimental testing, design processes, and optimisation studies, along with the latest developments in numerical modelling techniques. The review begins with an overview of vibration mitigation methods
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Review of sensor tasking methods in Space Situational Awareness Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-06-14 Chenbao Xue, Han Cai, Steve Gehly, Moriba Jah, Jingrui Zhang
To ensure the secure operation of space assets, it is crucial to employ ground and/or space-based surveillance sensors to observe a diverse array of anthropogenic space objects (ASOs). This enables the monitoring of abnormal behavior and facilitates the timely identification of potential risks, thereby enabling the provision of continuous and effective Space Situational Awareness (SSA) services. One
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A review of fault management issues in aircraft systems: Current status and future directions Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-05-08 A. Zolghadri
The academic community has extensively studied fault management in dynamical and cyber-physical systems, leading to the development of various model-based and data-driven/learning-enabled methods. Although these advanced designs show promise for improving conventional practices in aircraft systems, there is a noticeable disparity between academic methodologies and the specific needs of the aviation
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Recent progress of efficient low-boom design and optimization methods Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-05-08 Zhonghua Han, Jianling Qiao, Liwen Zhang, Qing Chen, Han Yang, Yulin Ding, Keshi Zhang, Wenping Song, Bifeng Song
Reducing the sonic boom to a community-acceptable level is a fundamental challenge in the configuration design of the next-generation supersonic transport aircraft. This paper conducts a survey of recent progress in developing efficient low-boom design and optimization methods, and provides a perspective on the state-of-the-art and future directions. First, the low- and high-fidelity sonic boom prediction
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Review on the crashworthiness design and evaluation of fuselage structure for occupant survivability Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-22 Haolei Mou, Jiang Xie, Zhenyu Feng, Xiaopeng Shi
Crashworthiness is the ability of civil aircraft fuselage structure and internal systems to maximum protect the occupants’ safety in a crash or emergency landing event, and is an important embodiment of the civil aircraft safety, which can determine the occupant survivability to a certain extent. The crashworthiness is dominated by the crash response characteristics of typical fuselage section (including
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Discontinuous Galerkin methods for hypersonic flows Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-18 Dominique S. Hoskin, R. Loek Van Heyningen, Ngoc Cuong Nguyen, Jordi Vila-Pérez, Wesley L. Harris, Jaime Peraire
In recent years, high-order discontinuous Galerkin (DG) methods have emerged as an attractive approach for numerical simulations of compressible flows. This paper presents an overview of the recent development of DG methods for compressible flows with particular focus on hypersonic flows. First, we survey state-of-the-art DG methods for computational fluid dynamics. Next, we discuss both matrix-based
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On the use of hybrid shock absorbers to increase safety of commercial aircraft passengers during a crash event Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-15 Antonio Garofano, Valerio Acanfora, Aniello Riccio
the passive safety of aircraft passengers is such an important aspect in the design of aircraft structures as strength and fatigue concerns. The development of methods and devices to prevent passenger injuries is the subject of continuous efforts. The mission is to minimize stresses and accelerations on passengers during a crash. Over the years, studies on crash phenomena have been focused on experimental
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Research progress in aero-optical effects of supersonic turbulent shear layers Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-15 Hao-lin Ding, Zi-hao Xia, Shi-he Yi, Qiong Gao, Tian Jiang
Aero-optical effects have received increasing attention in recent decades with the continuous development of high-speed missiles’ imaging guidance systems, airborne laser systems, and laser communication systems. Numerous experiments and engineering practices have shown that the aero-optical effects of the supersonic turbulent shear layer can reveal the essential characteristics of general aero-optical
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Cooperative motion planning and control for aerial-ground autonomous systems: Methods and applications Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-12 Runqi Chai, Yunlong Guo, Zongyu Zuo, Kaiyuan Chen, Hyo-Sang Shin, Antonios Tsourdos
This review article offers an in-depth analysis of cooperative motion planning and control in aerial-ground autonomous systems, emphasizing their methods and applications. It explores the integration of unmanned aerial vehicles (UAVs) and unmanned ground vehicles (UGVs), focusing on their synchronized planning and control mechanisms that enable efficient task execution in various settings, such as
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Country-first domestic satellites: A family tree Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-11 Maximilien Berthet, Shinichi Nakasuka, Mengu Cho, Kojiro Suzuki
The history of satellite development is at an inflection point: around half of all countries have made and launched satellites, while another half has not. In this context, the time appears right to take stock of lessons learnt from the development of country-first domestic satellites. These are defined as the first to have been designed, assembled, integrated, and/or tested with significant input
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Experimental characterization of the crashworthiness of carbon fiber reinforced epoxy composites Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-10 Maria Rosaria Ricciardi, Ilaria Papa, Valentina Lopresto, Andrea Calzolari, Lorenzo Vigna, Vincenza Antonucci
The crashworthiness of a structure is a measure of its protective capability under dynamic events by absorbing the crash energy in a controlled way. Fiber reinforced composite materials can represent a valid alternative to ductile metals as impact energy absorbers in a crashworthy structure. In fact, composites are characterized by high mechanical properties coupled with low weight, capability to be
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Impact response and crashworthy design of composite fuselage structures: An overview Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-09 Xiaochuan Liu, Chunyu Bai, Xulong Xi, Sicong Zhou, Xinyue Zhang, Xiaocheng Li, Yiru Ren, Jialing Yang, Xianfeng Yang
Airplanes are inevitably subjected to various impact loading conditions in the event of emergency landing. An airplane crash scenario is a complex nonlinear impact event which involves large deformation, material fracture, structural failure, and dynamic contact. The impact response becomes more complicated due to the presence of composite materials, which are becoming the dominated choice for aircraft
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Crashworthiness design and evaluation of civil aircraft structures Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-04-09 Valentina Lopresto
One of the most critical air transportation issues is the passengers' protection during collision and impact events that must be absorbed in a controlled way in order to reduce damages. The capability of an aircraft to eliminate injuries in relatively mild impacts and to reduce severe effects on occupants in critical crashes is called crashworthiness. The crashworthiness is the ability of a structure
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On the need to reassess the design tools for active flow control Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-29 Israel Wygnanski
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Slat noise in high-lift systems Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-18 Yang Zhang, Louis Cattafesta, Kyle Pascioni, Meelan Choudhari
This paper reviews several decades’ worth of research on the topic of slat noise arising from high-lift systems of commercial aircraft. A high-lift system is commonly used for providing additional lift by deploying the leading-edge slat(s) and trailing-edge flap(s) during the takeoff and landing phases of flight. Slat noise can be one of the main sources of airframe noise, along with the deployed landing
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Machine learning algorithms for delaminations detection on composites panels by wave propagation signals analysis: Review, experiences and results Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-14 E. Monaco, M. Rautela, S. Gopalakrishnan, F. Ricci
Performances are a key concern in aerospace vehicles, requiring safer structures with as little consumption as possible. Composite materials replaced aluminum alloys even in primary aerospace structures to achieve higher performances with lighter components. However, random events such as low-velocity impacts may induce damages that are typically more dangerous and mostly not visible than metals. The
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Supersonic transport optimization concepts Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-05 Dennis M. Bushnell
Review and discussion of substantive to revolutionary concepts to enable a commercially viable, societally acceptable supersonic transport. Issues addressed include economic viability, take off noise, sonic boom, emissions and frontier aircraft configurations. Solution spaces include an enabler for most of the issues, which is doubling the lift-to-drag ratio. Approaches in most cases require serious
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Flapping rotary wing: A novel low-Reynolds number layout merging bionic features into micro rotors Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-01 Long Chen, Cheng Cheng, Chao Zhou, Yanlai Zhang, Jianghao Wu
Since the birth of bio-inspired flapping-wing micro air vehicles, a controversial topic, i.e., whether and to what extent a flapping wing can outperform conventional micro rotors, has existed in the field of micro-to pico-scale unmanned aircraft. However, instead of answering this debate, an alternative idea that combines the flapping-wing and rotary-wing layouts was proposed and has been extensively
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Thin-walled deployable composite structures: A review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-03-01 Tian-Wei Liu, Jiang-Bo Bai, Nicholas Fantuzzi, Xiang Zhang
The elastic strain energy-driven thin-walled deployable composite structures, characterized by their integration of structure and functionality, have attracted considerable attention in the field of space applications. These structures utilize the stored strain energy accumulated during the folding process to achieve elastic deployment. Significant progress has been made in the understanding of deformation
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Designing high aspect ratio wings: A review of concepts and approaches Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-02-22 Yiyuan Ma, Ali Elham
In response to escalating environmental concerns and stringent economic constraints, there is an urgent need to develop aircraft technologies and configurations that substantially enhance efficiency. A prominent trend in aircraft design aimed at minimizing lift-induced drag, improving fuel efficiency, and mitigating emissions is the adoption of increased wing Aspect Ratio (AR). This paper examines
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Review of path planning in prospective multi-target active debris removal missions in low earth orbits Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2024-01-29 Andrey A. Baranov, Dmitriy A. Grishko
Trends in space technology development and rapidly increasing traffic in outer space are likely to lead to the emergence of a market for services for the removal of large debris objects to disposal orbits. The commercial benefits of Active Debris Removal missions are possible when multiple objects are removed by a single spacecraft-collector that flies between targets in an optimal sequence, trying
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Artificial Intelligence for Trusted Autonomous Satellite Operations Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-12-27 Kathiravan Thangavel, Roberto Sabatini, Alessandro Gardi, Kavindu Ranasinghe, Samuel Hilton, Pablo Servidia, Dario Spiller
Recent advances in Artificial Intelligence (AI) and Cyber-Physical Systems (CPS) for aerospace applications have brought about new opportunities for the fast-growing satellite industry. The progressive introduction of connected satellite systems and associated mission concepts is stimulating the development of intelligent CPS (iCPS) architectures, which can support high levels of flexibility and resilience
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Thermal management challenges in hybrid-electric propulsion aircraft Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-12-08 Majid Asli, Paul König, Dikshant Sharma, Evangelia Pontika, Jon Huete, Karunakar Reddy Konda, Akilan Mathiazhagan, Tianxiao Xie, Klaus Höschler, Panagiotis Laskaridis
The utilization of hybrid electric propulsion concept in aviation offers a viable solution to address the limitations posed by the relatively low energy density of batteries in fully electric aviation. These hybrid systems enable the aircraft to achieve a significant range while simultaneously minimizing carbon emissions. While the individual components of a Hybrid Electric Propulsion (HEP) system
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A review of the shock-dominated flow in a hypersonic inlet/isolator Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-11-18 He-xia Huang, Hui-jun Tan, Fang-bo Li, Xue-bin Tang, Yuan Qin, Li-Bin Xie, Yao-Yu Xu, Can-min Li, Si-min Gao, Yue Zhang, Shu Sun, Dan Zhao
A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of shocks, which induces complex internal flows. This paper comprehensively reviews the recent research achievements, focusing on the shock-dominated internal flow of an inlet/isolator. Considering the specific geometrical feature of the hypersonic inlet, the shock wave/boundary layer interactions (SWBLIs) are
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Additive manufacturing in the new space economy: Current achievements and future perspectives Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-11-17 T. Ghidini, M. Grasso, J. Gumpinger, A. Makaya, B.M. Colosimo
In recent years, the realm of space exploration has undergone a transformative shift, marked by the emergence of a thriving new space economy. This evolution has not only redefined existing space infrastructures and services but has also democratized access to space, accelerating exploration endeavors. At the core of such evolution is additive manufacturing (AM), a groundbreaking technology that has
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Standing oblique detonation for hypersonic propulsion: A review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-31 Zonglin Jiang
Standing oblique detonation is a unique pressure-gain combustion phenomenon for hypersonic ramjet propulsion, and its research has been related with supersonic combustion in scramjet engines since its births, for example, absent treatment in its early stage and re-consideration in recent decades. Standing oblique detonations and supersonic combustion share the same features of supersonic chemically-reacting
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Screening of metal fuels for use in composite propellants for ramjets Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-27 O.G. Glotov
A review of the literature on the methods for activation of the combustion of metallic fuels, mainly boron-containing ones, as the promising components of composite propellants for ramjets is presented. Some methods and ideas were checked experimentally using a laboratory approach developed for comparing the metallic fuels (MF) of different origin. The approach implies the determination of the set
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Ramjets/scramjets aerodynamics: A progress review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-27 Dan Zhao
Abstract not available
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On the importance of studying asteroids: A comprehensive review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-27 M. Azadmanesh, J. Roshanian, M. Hassanalian
This comprehensive study delves into the significance of asteroid research and proposes a systematic classification consisting of seven distinct categories. Initially, a concise definition is presented to differentiate between asteroids, meteorites, and comets, accompanied by a brief exploration of their unique characteristics. Recognizing the valuable scientific insights that these celestial bodies
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A review of three-dimensional shock wave–boundary-layer interactions Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-24 Kshitij Sabnis, Holger Babinsky
The vast majority of shock wave–boundary-layer interactions in practical applications like supersonic aircraft intakes are three dimensional in nature. The complex behaviour of such interactions can generally be understood by combining the flow physics of a limited number of canonical cases. The physical understanding of these flow fields developed by numerous investigators over the last half century
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Model validation hierarchies for connecting system design to modeling and simulation capabilities Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-25 James M. Luckring, Scott Shaw, William L. Oberkampf, Rick E. Graves
Hierarchical structures provide a means to systematically deconstruct an engineering system of arbitrary complexity into its subsystems, components, and physical processes. Model validation hierarchies can aid in understanding the coupling and interaction of subsystems and components, as well as improve the understanding of how simulation models are used to design and optimize the engineering system
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Review on the aerodynamic issues of the exhaust system for scramjet and turbine based combined cycle engine Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-22 Zheng Lv, Jinglei Xu, Guangtao Song, Rui Li, Jianhui Ge
A review of research progress in the design of the exhaust system for the scramjet and turbine based combined cycle (TBCC) engine is presented. Firstly, the technical challenges encountered in designing the exhaust system for a hypersonic propulsion system are highlighted and discussed, and the performance parameter definition as well as the theoretical thrust prediction for the exhaust system is introduced
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A holistic review of the current state of research on aircraft design concepts and consideration for advanced air mobility applications Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-10-03 Lukas Kiesewetter, Kazi Hassan Shakib, Paramvir Singh, Mizanur Rahman, Bhupendra Khandelwal, Sudarshan Kumar, Krishna Shah
Advanced Air Mobility (AAM) represents a collaborative vision shared by NASA, regulatory agencies, and global industry leaders, aimed at establishing a robust and reliable air transportation ecosystem, which is expected to facilitate safe and efficient movement of both people and cargo within urban, suburban, and regional environments. This paper presents a holistic review and analysis encompassing
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The prospects for green aviation by 2050 Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Max F. Platzer
The continued emission of greenhouse gases presents an existential threat to civilization on our planet. Although the aviation sector of the global economy contributes only a small percentage of the total greenhouse gas emissions it will become increasingly important to decarbonize this sector no later than 2050 if the danger of irreversible climate change is to be averted. In this special issue an
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Review of sustainable energy carriers for aviation: Benefits, challenges, and future viability Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Phillip J. Ansell
Sustainability has recently been identified as the greatest challenge facing the modern aviation field. Given the extreme power and energy characteristics of transport-class aircraft today,achieving sustainability goals across the aviation sector is a tremendous challenge when compared to other modes of transportation. Several key energy carriers have emerged, promising an environmentally sustainable
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The carbon dioxide challenge facing U.S. aviation and paths to achieve net zero emissions by 2050 Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Luke L. Jensen, Philippe A. Bonnefoy, James I. Hileman, Jay T. Fitzgerald
This paper investigates the potential pathways and associated requirements to meet a goal of net-zero greenhouse gas (GHG) emissions from the US commercial aviation sector by 2050 as outlined in the US 2021 Aviation Climate Action Plan. Aviation traffic (RTK) is projected to grow at an average of 2.0% per annum between 2019 and 2050, suggesting that a progressive and ultimately total decoupling of
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An open thinking for a vision on sustainable green aviation Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Antonio Ficca, Francesco Marulo, Antonio Sollo
The main goal of this paper is to present a vision for the future of aviation. Developing such a vision is always a complex matter, but in times of environmental emergencies and unjustifiable wars it becomes even more difficult. One of the main reasons of this paper is to show that there is still room for advancing clean technology developments and to demonstrate that the aviation sector is ready for
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Hydrogen-powered aircraft: Fundamental concepts, key technologies, and environmental impacts Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Eytan J. Adler, Joaquim R.R.A. Martins
Civil aviation provides an essential transportation network that connects the world and supports global economic growth. To maintain these benefits while meeting environmental goals, next-generation aircraft must have drastically reduced climate impacts. Hydrogen-powered aircraft have the potential to fly existing routes with no carbon emissions and reduce or eliminate other emissions. This paper is
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Review of hybrid-electric aircraft technologies and designs: Critical analysis and novel solutions Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Karim Abu Salem, Giuseppe Palaia, Alessandro A. Quarta
Reducing greenhouse gas emissions has become a priority for civil transport aviation. One of the possible solutions investigated by current aeronautics research is the introduction of electric propulsion, which would drastically reduce greenhouse gas emissions related to flight. This paper addresses this topic in depth; the work is structured in two intertwined parts. The first relates to an extensive
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Review of the hybrid gas - electric aircraft propulsion systems versus alternative systems Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Agata Kuśmierek, Cezary Galiński, Wieńczysław Stalewski
The continuously increasing interest in alternative aircraft propulsion systems is caused by the requirements and demands set by international institutions and government organizations. For instance, nowadays in the European Union, the objective called the European Green Deal seems most demanding. According to this regulation, the members of the European Union should ensure the net zero emission of
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Challenges, prospects and potential future orientation of hydrogen aviation and the airport hydrogen supply network: A state-of-art review Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 Hursit Degirmenci, Alper Uludag, Selcuk Ekici, T. Hikmet Karakoc
The use of fossil fuels, which are employed to supply the energy needs of aircraft, is currently causing severe environmental concerns, placing pressure on the aviation industry and mandating specific action. Sustainable aviation fuels that would lessen the aviation industry's environmental effects are viewed as a potential substitute for fossil fuels. Hydrogen, a clean energy carrier, is regarded
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Sustainable aviation in the context of the Paris Agreement: A review of prospective scenarios and their technological mitigation levers Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-09-19 S. Delbecq, J. Fontane, N. Gourdain, T. Planès, F. Simatos
The sustainability of air transport is increasingly studied in relation to climate issues. The objective of this paper is to provide the key elements for assessing whether a given transition scenario for aviation could be considered as sustainable in the context of the Paris Agreement. Addressing this question relies on a broad range of concepts which are reviewed. First, ethical considerations related
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Engineering perspective on bird flight: Scaling, geometry, kinematics and aerodynamics Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-08-14 Tianshu Liu, Shizhao Wang, Hao Liu, Guowei He
From the perspective of aeronautical engineers, this paper gives a systematical summary of the technical aspects of bird flight that should be considered in the analysis and design of flapping unmanned and micro air vehicles (UAVs and MAVs). The relevant aspects include the scaling laws, avian wing geometry, avian wing kinematics, aerodynamics models, computations, and special topics. Instead of extensively
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Developments in pogo suppression methods for liquid rockets Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-07-20 Chujun Wu, Zongxia Jiao, Yuanzhi Xu, Jiuhui Hu, Hui Pan
Pogo is a longitudinal vibration of liquid rockets, which is considered as a fluid-structure coupling of liquid supply system and rocket's structure. Its suppression is a critical element in the design of the fluid piping systems in liquid rockets, for many of them have been reported suffering the pogo vibration worldwide. Pogo suppression is a systematic technology including fluid-structure modelling
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A perspective on the urgency for green aviation Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-07-19 Max F. Platzer
It has become apparent that the continued emission of greenhouse gases will lead to the onset of irreversible climate change, thereby endangering human civilization on our planet. Although the aviation sector of the global economy contributes only a small percentage of the total emissions the transition to emission-free (green) aviation will be a crucial part of the transition to a green global economy
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Recent progress on high-order discontinuous schemes for simulations of multiphase and multicomponent flows Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-06-28 Yu Lv, John Ekaterinaris
There have been growing research interests in high-order discontinuous schemes over recent years. With established theoretical basis and framework, more efforts have recently been taken to enable discontinuous-scheme capabilities for modeling complex multi-physical flows. Substantial achievements and milestones have been reached in the development of compatible numerical methods and algorithms that
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A review of water sublimation cooling and water evaporation cooling in complex space environments Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-06-22 Kaifeng Chang, Yu-Ying Wang, Yun-Ze Li
With the lunar base, crewed Mars exploration and other future exploration plans proposed, the thermal control system of spacecraft will face challenges such as significantly higher thermal load and more complex and variable thermal environment. Traditional radiant heat sinks can hardly cope with the more demanding heat rejection requirements brought by these challenges, and more efficient, reliable
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Recent advances in feature extraction techniques for high-speed flowfields Prog. Aerosp. Sci. (IF 11.5) Pub Date : 2023-06-18 S. Unnikrishnan
Space–time scale-resolved diagnostic and computational campaigns routinely produce high-fidelity multi-disciplinary truth-model quality datasets for complex configurations. The extraction of the primary features of engineering or scientific interest and modeling of potential low-rank dynamics has proven challenging because of the massive sizes of the databases. One approach to overcome these challenges