Wu / Liang | The Future Vision of Aerospace Engineering: Technological Evolution and Trend Analysis | Buch | 978-981-9203-96-3 | www.sack.de

Buch, Englisch, 687 Seiten, Format (B × H): 155 mm x 235 mm

Reihe: Springer Aerospace Technology

Wu / Liang

The Future Vision of Aerospace Engineering: Technological Evolution and Trend Analysis

Selected Contributions of 2025 5th International Conference on Mechanical, Aerospace and Automotive Engineering
Erscheinungsjahr 2026
ISBN: 978-981-9203-96-3
Verlag: Springer Verlag, Singapore

Selected Contributions of 2025 5th International Conference on Mechanical, Aerospace and Automotive Engineering

Buch, Englisch, 687 Seiten, Format (B × H): 155 mm x 235 mm

Reihe: Springer Aerospace Technology

ISBN: 978-981-9203-96-3
Verlag: Springer Verlag, Singapore


This book offers a comprehensive collection of selected peer-reviewed papers presented at the 5th International Conference on Mechanical, Aerospace, and Automotive Engineering. It offers a forward-looking perspective on the evolving landscape of Aerospace Engineering, with a focus on technological advancements and emerging trends. Covering an array of topics—including Aerospace Manufacturing and Maintenance, Unmanned Aerial Vehicle, Flight System, Dynamics and Controls, Aerospace propulsion, Unmanned Aircraft Systems, Airspace Control, Airspace Management. It is designed for readers with a solid background in Aerospace Engineering, providing an in-depth look at new technologies and methodologies that shape the future of the industry. It also focuses on the real-world applications of these advancements. It is a valuable reference for anyone seeking to stay updated with the rapidly evolving aerospace industry.

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Zielgruppe


Research


Autoren/Hrsg.


Weitere Infos & Material


Study on Aircraft Cabin Temperature Management Based on Co-simulation Approaches.- Research on the Flight Test Technology of Emergency Power Systems for Civil Aircraft.- Study on Aircraft Cabin Temperature Management Based on Co-simulation Approaches.- Comparison of Experimental Drag and Lift Coefficients for NACA 4412 Airfoil: Effects of a Rotating Cylinder with and without Ridges.- Simulation and Verification of VHF Navigation System Based on Matlab/Simulink.- Risk Control of TAWS Flight Test in Real Environment.- Research on Flight Test Methodology for Weather Radar Systems.- Study on ADS-B-Based Inter-Vehicle Spacing Control in Dual-Aircraft Formation.- Optimization Design Method for Civil Aircraft Flight Test Loading Scheme Based on Genetic Algorithm.- Flight Test Data-Driven Prediction of Aircraft Electronics Bay Ventilation Performance Degradation.- Research on Flight Test Methodology for Aircraft Cabin Ventilation.- Research on Airspeed Measurement Principle and Test Method of Optical Air Data System.- Comparative Study and Analysis of Civil Aircraft Stall Characteristics Optimization Based on Flight Test Verification and Wind Tunnel Experimental Data.- Design of flight test method for simulated electrical load system.- Stochastic Frontier Analysis (SFA)-Based Research and Analysis on Mass-Production Flight Test Efficiency for Civil Aircraft.- Computational Methodology for Load Equations Using Multivariate Linear Regression Analysis.- Research on Factors Influencing Flow Performance of Laminar Flow Components.- Study and Validation of Airworthiness regulations for Civil Aircraft Engine In-Flight Restart.- Research on Energy Management Strategy of Extended Range Mining Truck Based on PA-ECMS.- Research on engine restarting flight test technology in the scenario of all-engines flameout of civil aircraft.- Direction-Selective Vibration Suppression of a Locally Resonant Metamaterial Beam.- Statistical Data-Driven Optimization of Civil Aircraft Flight Inspection Procedures.- Study on Combustion Failure Monitoring Methods in Methanol-fueled Engines.-  Quantitative Assessment of the Magnus-Induced Lift in Laminar Flow Past a Rotating Cylinder.- Research on Terrain Screening Technology for Civil Aircraft TAWS Mode 2 Flight Test Based on Warning Prediction Model.- A method of Pilots' Cognitive behavior Recognition Based on Hidden Markov Model.- Task Performance Characterization Indicators and Prediction Model for Display and Control Layout Patterns in Aircraft Cockpits.- Research on Air Turbulence Intensity Rating Method for Civil Aircraft Flight Test.- Research on the Application of Unplanned Fuel Policy in Civil Aircraft Flight Testing.- Research on Flight Test Pilot Technique for Ice-Contaminated Horizontal Stabilizer Stall-0g Push-Over in Civil Aircraft.


Dr. Wu received his BEng (2011) and PhD (2016) in Aerospace Engineering from Nanjing University of Aeronautics and Astronautics and Beihang University, respectively. His research interests compassing Computational fluid dynamics (CFD), Aircraft/Engine Environmental Adaptation, Aerodynamics, flight dynamics and aeroelastics, Multi phase flows, Aviation meteorology, Parachute fluid structure interaction simulation, Helicopter aerodynamics and flight dynamics, and Wind turbine aerodynamics. He is currently a Professor of College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, China. He has won the prizes including the National High Level Young Talent, Top Young Talent Plan of Beihang University, etc. He is the author or co-author of more than 50 SCI articles papers. At present, He has been the Editor/Assoc. Editor of Journal of Propulsion Technology, Peer Review Journal of Solar & Photo energy Systems, OA Journal Membranes, etc.

Dr. Liang received his BEng (1987) and MSc (1990) in Solid Rocket Motor Design, and Ph.D. (2000) in Aerospace Propulsion Theory and Engineering from Beijing University of Aeronautics and Astronautics (BUAA), respectively. He was promoted to associated professor in 1995 and to full professor in 2002. His research interests cover a wide spectrum of topical areas focusing on combustion, flow, heat transfer, and design for solid and liquid rocket propulsion, and tank pressurization system dynamics for launch vehicles. He supervises domestic and foreign M.S. and Ph.D. students in the field of rocket propulsion. He is the author or co-author of more than 100 technical papers and was the recipient of several teaching and research awards from government organizations. At present, He is Secretary General of the Teaching Steering Committee of the Ministry of Education of China for Aeronautics and Astronautics, Vice-Chairman of China Aerospace Propulsion Technology Information Society and Associate Editor of Chinese Journal of Propulsion Technology. His research of interests mainly focus on the following: 1. Integrated study on rocket engine design, simulation, and optimization; 2. Experimental study on dynamic process of rocket engine ignition and combustion; 3. Study on dynamics of launch vehicle pressurization feed system; 4. Design and experimental study on attitude control and orbit maneuvering propulsion system for spacecraft.



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