Forebody shock control devices for drag and aero-heating reduction: A comprehensive survey with a practical perspective

MYM Ahmed, N Qin - Progress in Aerospace Sciences, 2020 - Elsevier
One key feature that distinguishes the flowfield around vehicles flying in supersonic and
hypersonic regimes is the bow shock wave ahead of forebody. The severe drag and …

Active control devices of spiked body for drag and heat flux reduction in supersonic/hypersonic flows: State-of-the-art review

Y Meng, Z Wang, W Huang, Y Niu, Z Xie… - … Communications in Heat …, 2024 - Elsevier
Blunt-nose body structures are widely used in vehicles for better heat distribution due to
supersonic/hypersonic flight. However, such a body shape contributes to an increase of …

Coupled investigation on drag reduction and thermal protection mechanism of a double-cone missile by the combined spike and multi-jet

Y Meng, L Yan, W Huang, C Ji, J Li - Aerospace Science and Technology, 2021 - Elsevier
Vehicles flying at supersonic/hypersonic speeds would encounter severe aerodynamic and
aerothermodynamic environment, and hypersonic vehicles would produce high pressure …

Hypersonic drag and heat reduction mechanism of a new hybrid method of spike, multi-row discs and opposing jets aerodynamic configuration

SE Vali, S Abbasi - International Journal of Heat and Mass Transfer, 2022 - Elsevier
In this study, the drag force and aerodynamic heating reduction capacity of a novel
combined spike root jet and multi-row disk (SRJ-MRD) model consisting of a blunt body, a …

Investigation of influence factors to the reduction of hypersonic blunt-body drag and aeroheating based on a spike-aerodisk-channel concept

Z Wang, S Fang, J Guo, Z Ni, Y Xu - Acta Astronautica, 2023 - Elsevier
By slotting an inlet at the head of the aerodisk, a channel through the spike, and the lateral
jet outlet at the middle of the spike, the blunt body with spike-aerodisk can further reduce its …

Fluid-thermal coupled investigation on the combinational spike and opposing/lateral jet in hypersonic flows

Y Meng, L Yan, W Huang, Z Wang - Acta Astronautica, 2021 - Elsevier
The drag reduction and thermal protection mechanism induced by the spike and its
combinations with jet strategy is investigated in the current study. A fluid-thermal coupled …

Investigation of drag and heat flux reduction induced by a novel combinational spike-aerodisk and channel concept for hypersonic blunt body

J Guo, S Fang, Z Wang, Z Ni, Y Xu - Acta Astronautica, 2023 - Elsevier
For the drag and heat flux reduction of hypersonic blunt body, a novel combinational spike-
aerodisk and channel concept has been proposed. The high pressure air behind the bow …

Role of the backward-facing steps at two struts on mixing and combustion characteristics in a typical strut-based scramjet with hydrogen fuel

C Li, X Chen, Y Li, O Musa, L Zhu, W Li - International journal of hydrogen …, 2019 - Elsevier
Scramjet is one of the most promising propulsion systems for the new generation
supersonic/hypersonic air-breathing flight vehicles. To achieve sufficiently high combustion …

Assessment on the supersonic combustor performance induced by the asymmetric struts with hydrogen fuel

C Li, Y Li, X Chen, L Zhu, Y Hou - International Journal of Hydrogen Energy, 2020 - Elsevier
Enhancing the combustion efficiency of gas fuel, ie, hydrogen, in supersonic reacting flows
has attracted wide attention around the world, besides, the flame holders are the key …

Drag and heat reduction mechanism induced by jet interaction over a reusable launch vehicle in hypersonic flows

Y Meng, Z Wang, Y Shen, W Huang, Y Niu, L Yan - Acta Astronautica, 2022 - Elsevier
This paper presents numerical analyses of lateral jets in hypersonic flow injected at the
blending area of a reusable launch vehicle. The simulation is performed utilizing the three …