Advances in Aerodynamics (AIA), focusing on rapid publication of comprehensive studies on the frontier of aerodynamics, aims 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 innovative 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), and Multi-disciplinary Related Aerodynamics (aeroacoustics, aeroelasticity, hydrodynamics, thermomechanics). AIA sincerely welcomes your original, high-quality and excellent manuscripts on aerodynamic research.
Advances in Aerodynamics
Description
Identifiers
e-ISSN | 2524-6992 |
Publisher
Springer Singapore
Additional information
Data set: Springer
Articles
Advances in Aerodynamics > 2019 > 1 > 1 > 1-6
For the general case of a spatial isoenergetic flow of ideal gas, Helmholtz’s theorems are generalized and the speed with which vortex tubes move is found, keeping the intensity. It is shown that along the streamline without stagnation point, vorticity either is equal to zero everywhere, or it is non zero at all. The pattern of vortex lines behind the three-dimensional detached bow shock wave is specified.
Advances in Aerodynamics > 2019 > 1 > 1 > 1-25
Weighted essentially non-oscillatory (WENO) schemes are a class of high-order shock capturing schemes which have been designed and applied to solve many fluid dynamics problems to study the detailed flow structures and their evolutions. However, like many other high-order shock capturing schemes, WENO schemes also suffer from the problem that it can not easily converge to a steady state solution if...
Advances in Aerodynamics > 2019 > 1 > 1 > 1-16
The numerical methods for computing the stability derivatives of the aircraft by solving unsteady sensitivity equations which was proposed in our previous papers was extended to solve three-dimensional problems in this paper. Both the static and dynamic derivatives of the hypersonic blunt cone undergoing pitching oscillation around a fixed point were computed using the new methods. The predicted static...