Forebody shock control devices for drag and aero-heating reduction: A comprehensive survey with a practical perspective
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 …
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 …
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 …
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 …
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 …
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 …
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 …
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
Scramjet is one of the most promising propulsion systems for the new generation
supersonic/hypersonic air-breathing flight vehicles. To achieve sufficiently high combustion …
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
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 …
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 …
blending area of a reusable launch vehicle. The simulation is performed utilizing the three …