Nearly all illuminating classic hypersonic flow theories address aerodynamic phenomena as a perfect gas in the high-speed range and at the upper limit of continuum gas domain. The hypersonic flow is quantitatively defined by the Mach number independent principle, which is derived from the asymptotes of the Rankine-Hugoniot relationship. However, most hypersonic flows encounter strong shock-wave compressions resulting in a high enthalpy gas environment that always associates with nonequilibrium thermodynamic and quantum chemical-physics phenomena. Under this circumstance, the theoretic linkage between the microscopic particle dynamics and macroscopic thermodynamics properties of gas is lost. When the air mixture is ionized to become an electrically conducting medium, the governing physics now ventures into the regimes of quantum physics and electromagnetics. Therefore, the hypersonic flows are no longer a pure aerodynamics subject but a multidisciplinary science. In order to better understand the realistic hypersonic flows, all pertaining disciplines such as the nonequilibrium chemical kinetics, quantum physics, radiative heat transfer, and electromagnetics need to bring forth. Read more.
Featured article: High-enthalpy hypersonic flows
Message from the Editors-in-Chief
On behalf of the editorial board, we are honored to announce the launch of a new journal, Advances in Aerodynamics (AIA), and we are very pleased to share with you our vision for the development of this journal. AIA is an international peer-reviewed open access journal which publishes high quality papers with originality, novelty, and significant contributions to the progress in aerodynamics. The journal will provide authors with an open and fair platform to promote their research and identify themselves in the aerodynamics community. Read more.
Aims and scope
Advances in Aerodynamics (AIA) is aimed to report the scientific and technological advances in aerodynamics from the aspects of academic research, industrial development and engineering applications, and to provide a platform for ideas exchange and discussion in this fast-changing field. The journal welcomes reviews and regular papers of novel studies on aerodynamic science and engineering. The topics include but are not limited to:
- Theoretical and Computational Aerodynamics
▪ Equilibrium and non-equilibrium flow
▪ Numerical method and validation
▪ Turbulent flow modeling and simulation
▪ Non-equilibrium and multi-physics flow simulation
- Aerospace Engineering Aerodynamics
▪ Aircraft research
▪ Aerodynamic analysis and design
▪ Propulsion and combustion
▪ Flow control
▪ Experimental aerodynamics
- Industrial Aerodynamics
▪ Innovative aerodynamic concept & Bio-inspired design
▪ Automobile and high-speed ground vehicle
▪ Renewable energy industries
▪ Environmental pollution
- Multi-disciplinary Related Aerodynamics
Advances in Aerodynamics is affiliated with the Chinese Aerodynamics Research Society, which is supported by China Aerodynamics Research and Development Center.
Chinese Aerodynamics Research Society (CARS) is a national, academic and non-profit social organization voluntarily formed by the academics practitioners and institutions engaged in aerodynamic research. It is also a constituent of China Association for Science and Technology.
Dedicated to promoting academic exchanges and scientific popularization in the field of aerodynamics in China, CARS has published several professional journals and organized activities such as Chinese Conference of Aerodynamics Annual Meeting, National Aeroelastic Academic Exchange Meeting, National Conference on Computational Fluid Dynamics.
Annual Journal Metrics
37 days to first decision for reviewed manuscripts only
30 days to first decision for all manuscripts
50 days from submission to acceptance
33 days from acceptance to publication
- ISSN: 2524-6992 (electronic)