Corpus ID: 10143742

Workshop " Thermochemical processes in plasma aerodynamics " Analysis of Scramjet with NHD bypass

@inproceedings{SheikinWorkshopT,
  title={Workshop " Thermochemical processes in plasma aerodynamics " Analysis of Scramjet with NHD bypass},
  author={Evgeniy Sheikin}
}
The propositions to use the MHD systems to control flow in a scramjet channel were put forward in development of the "AJAX" concept. The paper [1], in which the basic principles for the MHD control in a scramjet were described for the first time in detail, was published in 1998. The main emphasis in the paper was put on analyzing the scramjet scheme with the control system composed of the MHD generator located upstream of the combustion chamber and the MHD accelerator located downstream of the… Expand

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References

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Use of MHD systems in hypersonic aircraft
The possibilities of using magnetohydrodynamic (MHD) systems on hypersonic aircraft are discussed. The distinctive features of using MHD systems in the flow path of ramjet engines are examined. AExpand
Scramjet with MHD control under "Ajax" concept - Physical limitations