A review of parametric approaches specific to aerodynamic design process

T Zhang, Z Wang, W Huang, L Yan - Acta Astronautica, 2018 - Elsevier
Parametric modeling of aircrafts plays a crucial role in the aerodynamic design process.
Effective parametric approaches have large design space with a few variables. Parametric …

Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact

GJ Dominguez Calabuig, L Miraux, AR Wilson… - Proceedings of the 9th …, 2022 - arpi.unipi.it
Reusable launch vehicles (RLV) are slowly emerging as a solution to reduce space access
costs, bring ing potential benefits from novel breakthrough space application. Whilst space …

Multidisciplinary design optimization of a wide speed range vehicle with waveride airframe and RBCC engine

T Zhang, X Yan, W Huang, X Che, Z Wang - Energy, 2021 - Elsevier
The wide speed range vehicle is believed to be ideal for space round trip and its design
process incorporates a number of disciplines. To achieve an overall optimal design, we …

Design and analysis of the air-breathing aircraft with the full-body wave-ride performance

T Zhang, X Yan, W Huang, X Che, Z Wang… - Aerospace Science and …, 2021 - Elsevier
Waverider is expected to break the lift-to-drag ratio constraint in the hypersonic flight
condition and it is commonly been studied as the forebody of the cruise vehicle. In this …

Parameterization and optimization of hypersonic-gliding vehicle configurations during conceptual design

T Zhang, Z Wang, W Huang, L Yan - Aerospace Science and Technology, 2016 - Elsevier
Three-dimensional class/shape function transformation (CST) approach is an analytical
method, and it can define the geometrical shapes by a small number of parameters and it is …

A design approach of wide-speed-range vehicles based on the cone-derived theory

T Zhang, Z Wang, W Huang, S Li - Aerospace Science and Technology, 2017 - Elsevier
The hypersonic gliding vehicle is attracting an increasing attention because of its high lift-to-
drag ratio and cruising velocity. This kind of vehicle may experience different airspaces as …

A study of performance parameters on drag and heat flux reduction efficiency of combinational novel cavity and opposing jet concept in hypersonic flows

X Sun, Z Guo, W Huang, S Li, L Yan - Acta Astronautica, 2017 - Elsevier
The drag reduction and thermal protection system applied to hypersonic re-entry vehicles
have attracted an increasing attention, and several novel concepts have been proposed by …

Research status and development trend of air-breathing high-speed vehicle/engine integration

S Luo, Y Sun, J Liu, X Xie, J Tian, J Song - Aerospace Science and …, 2024 - Elsevier
Air-breathing vehicles, a crucial field of the aerospace industry in recent years, are required
to have exceptional flight performance in a wide range. As a practical and essential way to …

Design and investigation on variable Mach number waverider for a wide-speed range

S Li, Z Wang, W Huang, J Lei, S Xu - Aerospace Science and Technology, 2018 - Elsevier
A design methodology of the variable Mach number waverider is proposed for the wide-
speed range vehicle in this paper. The proposed approach is based on the variable design …

Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator

A Viviani, L Iuspa, A Aprovitola - Aerospace Science and Technology, 2017 - Elsevier
In this paper we developed a multi-disciplinary, multi-objective optimization procedure for
the shape generation of re-entry spacecrafts performing conventional landing from a Low …