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• Distinct Dynamics of Lithium Intercalation and Plating on Graphite Anode of Li-Ion Batteries for eVTOL Applications
  Electrifying air mobility is a major move toward cleaner, more efficient transportation. Li-ion batteries are poised to play a crucial role in achieving this goal by powering the electric vertical take-off and landing (eVTOL) platforms 1, 2 . Unlike Li-ion bat…
  crossref Muhammad Mominur Rahman, Ruhul Amin, Ali Abouimrane, Ilias Belharouak 2025-11-24T07:48:08Z 置信度 0.70
• Determination of Aircraft Design Parameters
  crossref Nikolai K. Liseitsev 2025-08-31T15:17:33Z 置信度 0.70
• A Novel Topology With the Combination of Superconducting Magnet and Permanent Magnet for the Propulsion Motor of eVTOL Aircraft
  crossref Xinhong Gao, Yuanzhi Zhang, Haiyang Fang, Dawei Li 等 2025-02-13T18:50:33Z 置信度 0.70
• Conceptual Design of Aircraft System Routing Architectures Using a Bio-Inspired Algorithm
  The increasing complexity of aircraft systems and the shift toward electrical aircraft are driving the introduction of entirely new concepts in aircraft systems and airframe design; it is therefore likely that the evaluation of aircraft systems and their integ…
  crossref Jumpei Taneich, Kenichi Rinoie 2024-12-17T14:51:41Z 置信度 0.70
• Vibration and Noise Analyses of eVTOL Tilting Propeller with Different Anhedral Angles in Low-Speed Flight
  Abstract. In this study, a notional eVTOL tiltrotor model is developed and analyzed using the rotorcraft comprehensive analysis code, CAMRAD II, to investigate the effects of blade tip anhedral angles (Γ = 0°, 15°, and 25°) on hover performance, rotor hub vibr…
  crossref Gi-Jeong Park 2026-07-09T16:00:12Z 置信度 0.70
• Induced flow measurements and analytical tonal noise predictions for a sub-scale eVTOL rotor
  Tonal acoustic predictions of a fixed pitch rotor in edgewise flight are developed based on rotor inflow measurements. The induced velocity of a fixed-pitch rotor in hover and edgewise flight was measured with stereoscopic particle image velocimetry (sPIV) in …
  crossref James Goldschmidt, Lawrence Ukeiley 2025-09-30T05:42:37Z 置信度 0.70
• A Power-Following Energy Management Strategy for Hydrogen-Electric Hybrid eVTOL
  crossref Qi Pengfei, Li Yong, Zhang Kaixuan, Chen Sheng 等 2026-01-20T20:37:18Z 置信度 0.70
• Hybrid Renewable Power Integration (Solar+Wind+Thermal+Microwave + Fuel Cell) in eVTOL and Satellites
  This research explores the intelligent integration and optimal scheduling of hybrid renewable energy sources—solar, wind, thermal, microwave, and fuel cell—for electric vertical take-off and landing (eVTOL) aircraft and satellite systems. With growing interest…
  crossref Adnan Haider Zaidi 2025-06-24T18:09:12Z 置信度 0.70
• Key-Based Authentication Scheme for Evtol Drones Using Chebyshev Chaotic Maps
  crossref Eduardo Hernandez Escobar, Muhammad Zain Chaudhary, Hosameldin Darwish, Ahmed Sherif 等 2025-09-08T17:38:33Z 置信度 0.70
• A Model for the Scheduling of Commercial eVTOL Flights Considering Grid Restrictions
  crossref Eduardo Castillo Fatule, Fengyu Wang, Di Shi, Zhenping Guo 等 2025-12-09T18:31:53Z 置信度 0.70
• Two-Dimensional Static Margin for Three-Dimensional Aircraft
  crossref David K. Schmidt, Derek Lisoski, Brian P. Danowsky 2025-02-20T11:20:51Z 置信度 0.70
• Hydrodynamic performance and maneuverability design for a compound eVTOL configuration based unmanned aerial underwater vehicle
  crossref Hangyu Zhou, Zhaoyu Wei, Weiqiang Hu 2025-01-02T06:28:02Z 置信度 0.70
• Simulation-Based Evaluation of Motor Failure Resilience in a Prototyped Multirotor eVTOL
  This study investigates the fault tolerance of a large-scale coaxial quadrotor Electric Vertical Takeoff and Landing (eVTOL) under motor failure through high-fidelity software-in-the-loop (SIL) simulations using PX4-Gazebo environment. The objective is to eval…
  crossref Mostafa Asadi Khanouki, Younes Sadat-Nejad, Nima Pourmostaghimi 2025-07-02T17:29:17Z 置信度 0.70
• A data-driven method for aircraft static strength test anomaly recognition
  The strain data from the static strength test of the aircraft is the correct response to the structure bearing deformation. Real-time monitoring and fast analysis of strain data is an important factor. In this paper, we propose a data-driven approach for aircr…
  crossref Jiaojiao Chen, Chang Liang, Xiaohua Nie 2025-04-23T14:28:51Z 置信度 0.70
• Energy-Harvesting Performance of an Aircraft Propeller
  The electrification of aircraft is strongly coupled with the use of propellers as a propulsion system because of their high efficiency and their convenient integration with electric motors. Due to the operational flexibility of electric motors, the propeller c…
  crossref Robert Nederlof, Daniele Ragni, Tomas Sinnige 2025-03-10T07:51:06Z 置信度 0.70
• Noise of a Propeller Designed for eVTOL Operations in Forward and Edgewise Flight
  The performance and acoustics of a scaled propeller designed for an eVTOL vehicle were investigated in axial and edgewise flight. The measured performance compared well with BEMT predictions in axial flight conditions. The noise produced by the propeller is do…
  crossref Szu-Fu Huang, Shreyas Chaware, Ryan Lundquist, Nanyaporn Intaratep 等 2026-04-10T16:56:52Z 置信度 0.70
• Commercial Aircraft
  crossref Scott Jackson 2025-05-15T13:31:32Z 置信度 0.70
• Dynamic Drop Testing of eVTOL Energy Storage Systems Part 2: Deformation and Post-Test Forensics Results
  Researchers at the National Aeronautics and Space Administration (NASA) have conducted a series of module-level 50-ft dynamic drop tests on electric Vertical Take-off and Landing (eVTOL) Energy Storage Systems (ESS) for the generation of dynamic impact data to…
  crossref Shay Ellafrits, Nathaniel Gardner, Justin Littell 2026-04-10T16:56:52Z 置信度 0.70
• Aircraft Geometry and Propulsion Architecture Visualization for the Future Aircraft Sizing Tool (FAST)
  crossref Nawa Khailany, Paul Mokotoff, Gokcin Cinar 2025-02-12T09:44:16Z 置信度 0.70
• About Aircraft Weight Analysis (Weight Design)
  crossref Nikolai K. Liseitsev 2025-08-31T15:17:35Z 置信度 0.70
• A Semi-Analytical Multi-Objective Optimization of Outer-Rotor PM Machines for eVTOL Propulsion Systems
  crossref Zhe Guo, Xinggang Fan, Yongze Miao, Dawei Li 等 2025-12-30T18:35:19Z 置信度 0.70
• Active vibration control method based on rotor speed modulation for eVTOL
  crossref Kai Guan, Yang Lu, Changtian Wang, Jinru Chen 2025-04-11T07:03:28Z 置信度 0.70
• Aerodynamic Analysis of Stopped and Stopping Rotors in Lift+Cruise eVTOL Configurations
  This study investigates the aerodynamic behavior of lift rotors in a representative lift+cruise electric vertical takeoff and landing (eVTOL) configuration using high-fidelity Computational Fluid Dynamics (CFD) simulations. As lift+cruise concepts gain promine…
  crossref Koushik Marepally, James Baeder, Zoren Habana, Jan Goericke 等 2026-04-10T16:56:52Z 置信度 0.70
• Experimental investigation of vortex ring state in an eVTOL propeller
  crossref Alberto Savino, Andrea Gianotti, Giovanni Droandi, Mike Kerho 等 2025-06-13T12:03:27Z 置信度 0.70
• A Physical-Data Hybrid Method of Multi-Fault Diagnosis for eVTOL Under Closed-Loop Control
  crossref Han Wang, Xin Wang, Danyang Han 2025-11-19T18:43:08Z 置信度 0.70
• Taking unsustainability to new heights: eVTOL and the disasters to come
  crossref Peter E. Wells 2025-01-17T13:01:18Z 置信度 0.70
• Aerodynamic Design of Shock Control Bumps on an Aircraft Considering Structural Constraints
  Shock control bumps can reduce the overall drag of a modern transport aircraft by reducing the wave drag. In this study, different shapes of static shock control bumps on a laminar wing are aerodynamically analyzed using numerical tools. This design study intr…
  crossref Andreas Goerttler 2025-05-19T08:17:31Z 置信度 0.70
• Study of Advanced Occupant Models to Quantify Injury Risk for eVTOL Vehicles
  Urban transportation is currently evolving from traditional ground-based vehicles to include air-based electric vertical take-off and landing (eVTOL) vehicles. These new eVTOL vehicles are designed to be small, lightweight, and eventually autonomously operable…
  crossref Nathaniel L. Jones, Jacob Putnam, Costin Untaroiu 2025-06-24T01:05:50Z 置信度 0.70
• Flow Distortion in a Small Unmanned Aircraft Boundary Layer Ingestion Inlet
  Abstract This paper presents a flow distortion study for a small, unmanned aircraft engine inlet that ingests fuselage boundary layer flow at low subsonic speeds. Recent efforts to reduce commercial transport aircraft drag at high subsonic speeds include embed…
  crossref Tyler Zimbelman, Kurt Rouser 2025-08-11T14:09:08Z 置信度 0.70
• Flight Dynamics and Control Analysis for Motor Sizing and Failure Accommodation for a Lift+Cruise eVTOL Near Hover
  This paper demonstrates methods of aircraft sizing, flight dynamics modeling, and performance analysis using a lift+cruise concept vehicle with an electric powertrain and variable-speed rotors. The central focus is the development of methods to relate the airc…
  crossref David Hartman, Peter Suh, George Altamirano 2026-04-10T16:56:52Z 置信度 0.70
• Comparative economic, energy, and environmental analysis of fuel cell and electric eVTOL systems: Case study of Iberian Peninsula
  crossref Néstor Velaz-Acera, Rodrigo Ruiz-Marín, David Borge-Diez 2025-02-15T22:06:56Z 置信度 0.70
• Theoretical and Methodological Foundations of Aircraft Design
  crossref Nikolai K. Liseitsev 2025-08-31T15:17:36Z 置信度 0.70
• Experimental and Computational Evaluation of Particle Impact Dampers in Multi-Mode Passive Vibration Control of eVTOL Support Arms
  Electric vertical takeoff and landing aircraft (eVTOL) have swiftly risen to prominence since the early 2000's due to their potential to serve as a sustainable and scalable improvement in urban air mobility. In edgewise forward flight, these aircraft can exper…
  crossref Siddhant Sandeep Bapat, Edward Smith, Nicholas Vlajic 2026-04-10T16:56:52Z 置信度 0.70
• Editorial: Research and education in aircraft design
  crossref Tomasz Goetzendorf-Grabowski 2025-10-30T07:49:18Z 置信度 0.70
• Electric Aircraft Charging Evolution Lessons from Automotive Charging
  Electric Aircraft Charging Evolution Lessons from Automotive Charging
  crossref Joshua Portlock 2026-07-21T17:01:11Z 置信度 0.70
• On the Design and Testing of a Full-Scale Quiet and Efficient eVTOL Propeller
  This paper describes the design, development, and testing of a full-scale eVTOL propulsor optimized for quiet and efficient operation. To design the propulsor, a design tool was developed for predicting the aerodynamic and acoustic performance of eVTOL propell…
  crossref David Coleman, Joseph Heimerl, Atanu Halder, Eric Greenwood 等 2026-04-10T16:56:52Z 置信度 0.70
• Aircraft Pilot Assistance System: Detection of Other Aircraft Using Artificial Neural Networks
  Abstract The publication presents a pilot assistance system that is based on video camera frames and uses the developed 3AFPBBYOLO artificial neural network model. The model is able to determine the relative location of other aircraft in the vicinity of an air…
  crossref Paweł Tomiło 2025-04-17T15:00:47Z 置信度 0.70
• 2025 International Conference on Unmanned Aircraft Systems (ICUAS)
  crossref 2025-05-27T17:08:30Z 置信度 0.70
• Ground Vibration Testing of Very Flexible Aircraft
  As aircraft become more flexible in an effort to improve efficiency to reduce fuel consumption and operating costs and improve endurance, structural nonlinearities become more apparent. As a consequence, testing practices that are well established and mature f…
  crossref Bilal Sharqi, Carlos E. S. Cesnik 2025-07-31T11:12:22Z 置信度 0.70
• Inter-turn short circuit fault diagnosis methods for eVTOL propulsion motor based on back EMF harmonic analysis
  Abstract The faulty degree assessment and faulty phase detection method of eVTOL propulsion motors Inter-Turn Short-Circuit (ITSC) are proposed in this paper based on the back electromotive force (back EMF) characteristics. A sliding mode observer (SMO) is uti…
  crossref Jie Gao, Chengzhi Zou 2025-08-13T18:03:39Z 置信度 0.70
• Optimal Mission Profile for Low-Boom Supersonic Aircraft
  crossref Wu Li, Karl Geiselhart, Christopher Eggert 2025-02-13T04:15:48Z 置信度 0.70
• Metamodeling Approach for Wing Structural Sizing of Box-Wing Aircraft
  This paper presents a predictive metamodel, built on a finite element method (FEM)-based design of experiment (DoE), developed for the structural design of a box wing. For this configuration, statistical or semi-empirical predictions are not available for the …
  crossref Giuseppe Palaia, Karim Abu Salem, Vincenzo Binante, Erasmo Carrera 2025-02-17T04:04:51Z 置信度 0.70
• FAST: A Future Aircraft Sizing Tool for Conventional and Electrified Aircraft Design
  crossref Paul Mokotoff, Maxfield Arnson, Yi-Chih Wang, Gokcin Cinar 2025-02-12T10:03:43Z 置信度 0.70
• Design Features of Commercial Airliners and Cargo Aircraft
  crossref Valentin A. Kiselev 2025-08-31T15:17:32Z 置信度 0.70
• Guest editorial: Research and education in aircraft design
  crossref Tomasz Goetzendorf-Grabowski 2025-10-17T14:04:07Z 置信度 0.70
• Ride Quality in Transonic High-Aspect-Ratio-Wing Aircraft
  Evaluating human comfort during flight through a ride quality metric is critical to meeting aircraft operational requirements. This paper investigates the ride quality of a transonic high-aspect-ratio-wing aircraft, representative of a potential future commerc…
  crossref Divya Sanghi, Cristina Riso, Carlos E. S. Cesnik 2025-05-01T06:14:19Z 置信度 0.70
• Minimum-Power Trim of Overactuated Multi-Tiltrotor Aircraft in Transition
  Multi-tiltrotor aircraft concepts capable of vertical takeoff and landing along with efficient high-speed cruise often incorporate multiple propulsors, aerodynamic lifting surfaces, and control surfaces. The trim problem for a configuration with more control a…
  crossref Daniel S. Sagan, Mark T. Lau, Brian J. German 2025-05-01T05:22:15Z 置信度 0.70
• A novel procedure to minimize the acoustic and environmental impact of eVTOL vehicles for intra-city mission profiles
  crossref Caterina Poggi, Giovanni Bernardini, Massimo Gennaretti 2025-12-26T07:16:13Z 置信度 0.70
• Energy Aware Coverage Planning for a QuadPlane small Uncrewed Aircraft System
  crossref Akshay Mathur, Ella Atkins 2025-05-27T13:05:08Z 置信度 0.70
• Designing Aircraft in a Way that Reduces Human Error
  The causes of most incidents and accidents are attributed to humans, even though they are based on aircraft design and configuration. This chapter emphasizes the critical need for error-proof design in aviation to reduce human errors in aircraft maintenance an…
  crossref Seref Demirci 2025-01-13T09:37:54Z 置信度 0.70
• Battery Optimization for Sustainable Aviation: A Comprehensive Analysis for Battery Electric Aircraft
  The aviation industry is entering a transformative era with the introduction of electrified aircraft, driven by the imperative to reduce reliance on legacy fossil fuels and to mitigate the industry’s environmental impact. Battery systems are an enabling techno…
  crossref Todd A. Spierling, Alexander Lynch, Thomas H. Bradley 2025-05-13T06:09:12Z 置信度 0.70
• Concurrent Value-Driven Optimization Problems Addressing Aircraft Design, Manufacturing, and Supply Chain
  In the last decades, several studies show how the concurrent evaluation of manufacturing and supply chain in the early design phase brings significant advantages to industries. In this frame, a value-driven methodology has been developed and applied in the aer…
  crossref Giuseppa Donelli, Nathalie Bartoli, Thierry Lefebvre, Luca Boggero 2025-05-01T05:38:08Z 置信度 0.70
• Experimental Investigation of Vortex Ring State Conditions for Archer Maker eVTOL Tilter Propeller
  This study experimentally explores the behavior of an isolated propeller of an electric vertical takeoff and landing (eVTOL) aircraft, a next-generation type of vehicle that combines the operational capabilities of both helicopters and airplanes, in vortex rin…
  crossref Alberto Savino, Andrea Gianotti, Donato Grassi, Luca Riccobene 等 2026-04-10T16:56:52Z 置信度 0.70
• Air-Space and Hypersonic Aircraft Design
  crossref Eduard N. Dudar, Valery P. Timoshenko 2025-08-31T15:17:34Z 置信度 0.70
• Exploration of Off-Design Performance for Hybrid Electric Regional Aircraft
  Most studies investigate hybrid electric aircraft by comparing their respective performance over their design mission. However, most missions flown are less demanding in terms of payload and/or range. Kerosene aircraft can adapt their fuel load, yet battery-eq…
  crossref Vincent O. Bonnin, Maurice F. M. Hoogreef 2025-04-09T16:40:12Z 置信度 0.70
• eVTOL flutter analyses in wingborne flight via ground vibration test data and actuator failure effects on stability
  crossref Francesco Saltari, Franco Mastroddi, Luca Pustina, Marcus V. G. Muniz 等 2025-07-25T15:15:40Z 置信度 0.70
• Configuration Estimation from Position Data of Civil Jet Aircraft for Noise Mapping
  This study presents a novel machine learning approach for estimating the flap and landing gear configurations of civil jet aircraft based on position data. Optimized for noise calculations, this method simplifies the estimation process by grouping various conf…
  crossref Jonas Meister, Stefan Schalcher 2025-04-25T09:08:43Z 置信度 0.70
• Design Features of Combat Maneuvering Aircraft
  crossref Mikhail A. Pogosyan, Dmitry Yu. Strelets 2025-08-31T15:17:35Z 置信度 0.70
• Aircraft Load Estimation Using Linear Parameter-Varying System-Based Hybrid Observers
  The hybrid loads observer has demonstrated its precision in estimating structural loads and wind disturbances in prior applications. This level of precision is attained by combining a high-fidelity physical, nonlinear flight dynamics model with a data-driven c…
  crossref Oliver Luderer, Frank Thielecke 2025-02-10T17:14:56Z 置信度 0.70
• Design Features of Hydro-Aviation Aircraft
  crossref Leonid G. Fortinov, Anas M. Hairov 2025-08-31T15:17:36Z 置信度 0.70
• Development of the Aspirated Kiel Probe
  crossref Haideng Zhang 2025-06-10T09:35:18Z 置信度 0.70
• Design of Hydrogen Solid Oxide Fuel Cells in Blended-Wing–Body Aircraft
  This paper presents the design methodology for integrating a hydrogen solid oxide fuel cell/gas turbine (SOFC/GT) propulsion system into a blended-wing–body (BWB) aircraft and tube-and-wing (T&W) configurations for 365 and 162 passengers. The design method…
  crossref Oi Ching Vanessa Chung, Khaled AlSamri, Jacqueline Huynh, Jack Brouwer 2025-02-13T02:30:46Z 置信度 0.70
• Research on Multi-Objective Optimization Method of eVTOL Connection Structure Based on Convolutional Neural Network and Dwarf Mongoose Optimization Algorithm
  This paper studied the fallable structure of the seat and floor connection of the 500kg multi-rotor manned electric vertical take-off and landing (eVTOL) aircraft. In view of the lack of research on fallable structures, especially for seat connection structure…
  crossref Xinyi Zhang 2025-07-02T08:08:21Z 置信度 0.70
• Retrofit Measures for Aircraft Noise Reduction: Simulation Benchmark and Impact Assessment
  DLR, German Aerospace Center, has developed a low-noise retrofit to reduce noise generation of a conventional midrange transportation aircraft, i.e., measures to the airframe and engine exhaust nozzle. Selected measures have been installed onboard of DLR’s fly…
  crossref Lothar Bertsch, Michael Pott-Pollenske, Felix Wienke, Joscha Kurz 等 2024-11-14T01:13:58Z 置信度 0.70
• Thermal Simulation of Air-Cooled PMSM with Novel Winding Structure and Specialized Cooling Design for eVTOL Applications
  For high-power-density permanent-magnet synchronous machine (PMSM) used in electric vertical takeoff and landing (eVTOL) aircraft, heat dissipation is challenging due to potential temperature rise, which may cause irreversible demagnetization of permanent magn…
  openalex Zhe Huang, Yingzhen Liu, Jing Ou, Dianguo Xu 2025-05-23 置信度 0.72 ThermalComputer scienceElectromagnetic coilMechanical engineeringElectrical engineering
• The concept of integrating unmanned aircraft into a single airspace with manned aircraft
  Remotely piloted aviation systems are a new component of the aviation system, which, based on the latest developments in the field of aerospace technologies, open up new and expand existing opportunities for civil/commercial applications, increase the level of…
  crossref Oleh Alieksieiev, Nikolai Tsybov 2026-04-10T11:55:26Z 置信度 0.70
• Theodorsen’s and Garrick’s Flutter Calculations: Revisited
  crossref Boyd Perry 2024-12-04T09:13:52Z 置信度 0.70
• Development of AI-Based Control Systems for Electric Vertical Take-Off and Landing (eVTOL) Vehicles
  crossref A Chandrashekhar, H.Mickle Aancy, Gottumukkala Santhi, ChunduriKiran Kumar 等 2026-02-18T21:13:43Z 置信度 0.70
• Multifidelity Rotor Wake Modeling with Uncertainty Quantification of Transitioning Tilt-Propeller Aircraft Performance
  A framework for efficient multifidelity modeling of tilt-propeller aircraft performance is developed, with an emphasis on accurate modeling of transition maneuvers between vertical and forward flight. Low- and midfidelity vortex models are used for the propell…
  crossref Racheal M. Erhard, Juan J. Alonso, Michael A. Cunningham 2025-02-10T12:14:56Z 置信度 0.70
• Enhanced Neural Network Model for Aircraft Flight Dynamics Prediction From Flight Test Data - Business Aircraft Application
  crossref Maxime Szymanski, Georges Ghazi, Ruxandra M. Botez 2025-02-12T10:03:43Z 置信度 0.70
• Aircraft Electrical Power Systems
  crossref 2025-12-19T21:25:28Z 置信度 0.70
• Resilience of the Aircraft System
  crossref Scott Jackson 2025-05-15T13:31:32Z 置信度 0.70
• Aircraft Pneumatic Power Systems
  crossref 2025-12-19T21:25:28Z 置信度 0.70
• Dataset for Reliability-Based Design Optimization of a Long-Range eVTOL Aircraft under Uncertain Mission Parameters
  This dataset contains all code and optimization algorithms used in the following publication: Damien M. Keijzer, Saullo G. P. Castro. "Reliability-Based Design Optimization of a Long-Range eVTOL Aircraft under Uncertain Mission Parameters". Preprint, 2026.
  openalex Damien Keijzer, Beyne, E., Buszek, M., Cuadrat-Grzybowski, M. 等 2026 置信度 0.72 Computer scienceCode (set theory)Robust optimizationOptimization problemEngineering
• Impact of Physics-Informed Features on Neural Network Complexity for Li-ion Battery Voltage Prediction in Electric Vertical Takeoff and Landing Aircrafts
  The electrification of vertical takeoff and landing aircraft demands high-fidelity battery management systems capable of predicting voltage response under aggressive power dynamics. While data-driven models offer high accuracy, they often require complex archi…
  datacite Ipek, Eymen, Hirz, Mario 2026 置信度 0.66 Systems and Control (eess.SY)FOS: Electrical engineering, electronic engineering, information engineeringFOS: Electrical engineering, electronic engineering, information engineering
• Preliminary Design and Performance Assessment of Electric VTOL Blended Wing Body Aircraft
  Aeronautics researchers have been seeking the solution for sustainable aviation for a long time and the research and development of electric Vertical Take Off and Landing (eVTOL) aircrafts to facilitate the Urban Air Mobility (UAM) and Regional Air Mobility (R…
  datacite Deepak Poudel, Bijay Pal 2023 置信度 0.66 Blended Wing Body; eVTOL; Regional Air Mobility; electric propulsion; aerodynamic assessment
• Preliminary Design and Performance Assessment of Electric VTOL Blended Wing Body Aircraft
  Aeronautics researchers have been seeking the solution for sustainable aviation for a long time and the research and development of electric Vertical Take Off and Landing (eVTOL) aircrafts to facilitate the Urban Air Mobility (UAM) and Regional Air Mobility (R…
  datacite Deepak Poudel, Bijay Pal 2023 置信度 0.66 Blended Wing Body; eVTOL; Regional Air Mobility; electric propulsion; aerodynamic assessment
• A Survey of Security Challenges and Solutions for Advanced Air Mobility and eVTOL Aircraft
  This survey reviews the existing and envisioned security vulnerabilities and defense mechanisms relevant to Advanced Air Mobility (AAM) systems, with a focus on electric vertical takeoff and landing (eVTOL) aircraft. Drawing from vulnerabilities in the avionic…
  openalex Ghazanfari, Mahyar, Sharifi, Iman, Wei, Peng, Dahle, Noah 等 2026 置信度 0.72 Cryptography and Security (cs.CR)FOS: Computer and information sciencesAvionicsBackdoorComputer security
• Design of the fuselage of the eVTOL aircraft with T700S/JC-02A composite materials for emergency medical services
  datacite Rodriguez, Renzo Hernan Guerrero 2025 置信度 0.66
• Simulation-Based Optimization and Evaluation of Urban Air Mobility
  Current mobility systems face increasing strain due to rapid urbanization and growing mobility demands, resulting in transportation bottlenecks, longer travel duration, and exacerbated ecological externalities. Urban Air Mobility (UAM), utilizing electric vert…
  datacite Wu, Hao 2025 置信度 0.66
• Hovering efficiency optimization of the cycloidal propeller with end plates
  Cycloidal propellers are known for their omnidirectional vectored thrust, enabling smooth transitions between hovering and forward flight, making them ideal for unmanned aerial vehicles (UAVs) and electric vertical take-off and landing (eVTOL) aircraft. Howeve…
  datacite Li, Han Zhen, Hu, Yu, Zhang, Lai, Sun, Hong Bo 等 2025 置信度 0.66 Fluid Dynamics (physics.flu-dyn)FOS: Physical sciencesFOS: Physical sciences
• Urban Air Mobility Vehicle Dataset
  <p>A wide array of electric vertical takeoff and landing (eVTOL) vehicles are in various stages of development. The addition of these vehicles to the Urban Air Mobility (UAM) market would provide more options for short to medium distance aerial transport…
  datacite Howard, Ryan, Wright, Ethan, Mudumba, Sai, Gunady, Nicholas I. 等 2021 置信度 0.66 mobilityaviationAeronautics and Astronautics EngineeringEconomicstransportation
• High-order direct numerical simulation of finite span wings
  A wide range of modern aerodynamics applications, such as unmanned aerial vehicles (UAV) and electric vertical takeoff and landing (eVTOL) aircraft, require accurate aerodynamic predictions in transitional Reynolds number regimes. However, current industry-sta…
  datacite Rinaldi, Joseph-Raffael, Vermeire, Brian 2025 置信度 0.66
• The QuadPlane Small Uncrewed Aircraft System
  Emerging Advanced Air Mobility (AAM) aircraft designs offer electric Vertical Take-Off and Landing (eVTOL) capability. Lift+Cruise configurations combine the efficiency of wing lift or "cruise" mode with a maneuverable vertical or “lift” mode for vertiport dep…
  datacite Mathur, Akshay 2025 置信度 0.66 Vertical Take-Off and Landing (VTOL)Lift+CruiseAdvanced Air Mobility (AAM)Uncrewed Aircraft Systems (UAS)Energy Efficient Flight Planning
• Optimization Studies for Aircraft Considering Propeller-Wing Interaction
  Environmental concerns and advances in battery technology are currently fueling a widespread growth of interest in electric aircraft. Additionally, the fundamentally different nature of electric motors, compared to combustion engines, allows designers to exper…
  datacite Chauhan, Shamsheer Singh 2020 置信度 0.66 Propeller-wing interactioneVTOLTrajectory optimizationAerodynamic shape optimizationMDO
• Numerical Study on Jet-Like Outwash Induced by Multi-Rotor eVTOLs and Engineering Approaches for Outwash Mitigation
  This study presents a comprehensive computational investigation of outwash phenomena generated by electric vertical takeoff and landing (eVTOL) aircraft, with particular emphasis on how rotor geometry and alignment shape hazardous airflow patterns at vertiport…
  datacite Chen, Yen-Chen, Chueh, Chih-Che 2025 置信度 0.66 Fluid Dynamics (physics.flu-dyn)FOS: Physical sciencesFOS: Physical sciences
• LAA3D: A Benchmark of Detecting and Tracking Low-Altitude Aircraft in 3D Space
  Perception of Low-Altitude Aircraft (LAA) in 3D space enables precise 3D object localization and behavior understanding. However, datasets tailored for 3D LAA perception remain scarce. To address this gap, we present LAA3D, a large-scale dataset designed to ad…
  datacite Wu, Hai, Tang, Shuai, Wang, Jiale, Zou, Longkun 等 2025 置信度 0.66 Computer Vision and Pattern Recognition (cs.CV)FOS: Computer and information sciencesFOS: Computer and information sciences
• DESIGN AND ANALYSIS OF CFRP CRASH TUBES FOR ENERGY ABSORPTION IN eVTOLS
  This study examines the design, analysis, and validation of carbon fibre-reinforced polymer (CFRP) crash tubes for energy absorption in electric vertical take-off and landing (eVTOL) aircraft seats, aiming to optimize configurations for enhanced passenger safe…
  datacite Dimassi, Adli, Marciniak, Roland, Bachem, Harald, Dietrich, Jan 2025 置信度 0.66 600 Technik
• Development and Validation of an Additively Manufactured Tilt-Wing Actuator for a Subscale eVTOL Demonstrator
  To support ongoing research into flight dynamics and control functions for (tandem) tilt-wing eVTOL aircraft, a subscale flight test demonstrator is being developed. Tilt-actuators are essential to achieve the tilt-wing’s key characteristics of VTOL capability…
  datacite Ott, L., May, M., Milz, D. 2025 置信度 0.66 eVTOL DemonstratorAdditive Manufacturing3D printingTilt-ActuatorTilt-Wing
• SmartFly - deployment of Electric Vertical Take-Off and Landing (eVTOL) aircraft for passenger transport in Saxony, Germany.
  datacite Bruehl, Robert, Fricke, Hartmut, Tober, Lisa Anna, Markmiller, Johannes 等 2023 置信度 0.66
• Safety Analysis of eVTOL Operations based on STPA
  Electric Vertical Take-Off and Landing (eVTOL) aircraft are expected to be quieter and more cost-effective than helicopters, offering major economic and social benefits through improved connectivity. Their adoption will require new ground infrastructure and ai…
  datacite Elizebeth, Mariat James, Chen, Shufeng, Badaoui, Halima El, Khastgir, Siddartha 等 2025 置信度 0.66 Systems and Control (eess.SY)FOS: Electrical engineering, electronic engineering, information engineeringFOS: Electrical engineering, electronic engineering, information engineering
• Joint Resource Estimation and Trajectory Optimization for eVTOL-involved CR network: A Monte Carlo Tree Search-based Approach
  Electric Vertical Take-Off and Landing (eVTOL) aircraft, pivotal to Advanced Air Mobility (AAM), are emerging as a transformative transportation paradigm with the potential to redefine urban and regional mobility. While these systems offer unprecedented effici…
  datacite Xiong, Kai, Yang, Chenxin, Qin, Yujie, Ma, Wanzhi 等 2025 置信度 0.66 Networking and Internet Architecture (cs.NI)Signal Processing (eess.SP)FOS: Computer and information sciencesFOS: Computer and information sciencesFOS: Electrical engineering, electronic engineering, information engineering
• Experimental investigation into the dynamic characteristics of a tilting multirotor system
  Urban Air Mobility (UAM) promises a transformative leap in urban transportation, with electric vertical take-off and landing (eVTOL) aircraft at the forefront. Pivotal in eVTOL flexibility, especially during transitional flight phases, are tilting rotors. Howe…
  datacite Sharma, Tanuj, Rezgui, Djamel, Titurus, Branislav 2024 置信度 0.66 FOS: Engineering and technologyeVTOL (Electric Vertical Take-Off and Landing), Experimental Modal Analysis (EMA), Finite Element Analysis (FEA), Rotorstructure interaction, Sequential Quadratic Programming (SQP)
• Real World Assets on-Chain Assistance Low-Altitude Computility Networks: Architecture, Methodology, and Challenges
  Low-altitude airspace is becoming a new frontier for smart city services and commerce. Networks of drones, electric Vertical Takeoff and Landing (eVTOL) vehicles, and other aircraft, termed Low-Altitude Economic Networks (LAENets), promise to transform urban l…
  datacite Luo, Haoxiang, Zhang, Ruichen, Liu, Yinqiu, Sun, Gang 等 2025 置信度 0.66 Networking and Internet Architecture (cs.NI)FOS: Computer and information sciencesFOS: Computer and information sciences
• Why UAM Needs Real-World Rotor Wake Data
  This paper underscores the need for real-world measurements of rotor downwash, outwash, and trailing wakes generated by eVTOL aircraft. As these vehicles operate in low-altitude urban environments, their complex aerodynamic effects raise safety concerns not ad…
  datacite Fantauzzi, Marco, AlHammadi, Talal, Jacob, Donald, Valente, Gianluca 2025 置信度 0.66
• Why UAM Needs Real-World Rotor Wake Data
  This paper underscores the need for real-world measurements of rotor downwash, outwash, and trailing wakes generated by eVTOL aircraft. As these vehicles operate in low-altitude urban environments, their complex aerodynamic effects raise safety concerns not ad…
  datacite Fantauzzi, Marco, AlHammadi, Talal, Jacob, Donald, Valente, Gianluca 2025 置信度 0.66
• Computing Longitudinal Dynamic Derivatives of a VTOL Aircraft Using CFD Simulations and Forced-Oscillation Model
  This study presents a comprehensive evaluation of dynamic aerodynamic derivatives during aircraft transition phases using advanced CFD simulations and forced oscillation testing. Two case studies are examined: a three dimensional fighter aircraft (Standard Dyn…
  datacite Nezhad, Ali Khosravani, Kosari, AmirReza, Askari, Rasoul 2025 置信度 0.66 Systems and Control (eess.SY)FOS: Electrical engineering, electronic engineering, information engineeringFOS: Electrical engineering, electronic engineering, information engineering
• Nonlinear Control Strategy and Sensor Data Processing for a Lift-to-Cruise Aircraft
  Aerial systems, including electric vertical take-off and landing (eVTOL) vehicles with fixed-wing configurations, present distinct challenges across various flight phases, encompassing hover and the transition to aerodynamic wingborne flight. Effectively addre…
  datacite Surmann, Denis, Weinert, Maximilian, Myschik, Stephan 2024 置信度 0.66
• Constrained Control Allocation With Continuous-Time Rate Constraints: Three-Dimensional Case
  This paper presents a novel quadratic programming (QP) approach for constrained control allocation that directly incorporates continuous-time actuator rate constraints without requiring slack variables. Over-actuated aircraft configurations, particularly preva…
  datacite Özkurt, Süleyman, Grimm, Adrian, Fichter, Walter 2025 置信度 0.66 Optimization and Control (math.OC)Systems and Control (eess.SY)FOS: MathematicsFOS: MathematicsFOS: Electrical engineering, electronic engineering, information engineering
• Occupant Protection for Legacy Rotorcraft
  Rotorcraft aviation has a high injury and fatality rate from what should be survivable crashes. Only 10% of the U.S. fleet are compliant with the latest regulations with respect to the Emergency Landing Dynamic Condition Rule (14 CFR 27/29.562). Regulators are…
  datacite Hellstrom, Ian 2025 置信度 0.66