The spike attached to the nose of the hypersonic vehicle appears to be the most effective
and simplest approach for the drag and heat flux reduction in supersonic/hypersonic flows …

Drag reduction and thermal protection is very important for hypersonic vehicles, and a
counterflowing jet and its combinations is one of the most promising drag and heat release …

开展航天器动力学与控制的研究在航天技术的发展中起到举足轻重的作用,
其目的在于发展有效的方法促使航天器在各阶段平稳可靠地运行. 航天器技术发展迅速 …

Numerical simulations of a 2D axisymmetric aerodisked nose cone in hypersonic flow are
conducted, and innovative techniques involving forward injection of the gas from the …

The thermal protection on the surface of hypersonic vehicles attracts an increasing attention
worldwide, especially when the vehicle enters the atmosphere at high speed. In the current …

When flying at supersonic or hypersonic speeds through the air, the drag and severe
heating have a great impact on the vehicles, thus the drag reduction and thermal protection …

Opposing jet has been proven as a feasible strategy to achieve drag and heat reduction in
hypersonic vehicles. In actual flight, the reduction efficiency of the drag and heat flux of …

The return and vertical landing of the first launch stage is a concept enabling reusable
launch systems and has been successfully applied by SpaceX with the Falcon 9. The Falcon …

Current design requirements are shaping advanced and efficient supersonic or hypersonic
aircraft concepts, capable of flying between distant parts of the globe within hours, and …

A 7-element rocket combustion chamber using GOX/GCH 4 as propellant has been modeled
and simulated to get a more comprehensive knowledge for combustion and heat transfer …