@article{(Open Science Index):https://publications.waset.org/pdf/10002314,
	  title     = {Thrust Vectoring Control of Supersonic Flow Through an Orifice Injector},
	  author    = {Ibrahim Mnafeg and  Azgal Abichou and  Lotfi Beji},
	  country	= {},
	  institution	= {},
	  abstract     = {Traditional mechanical control systems in thrust
vectoring are efficient in rocket thrust guidance but their costs
and their weights are excessive. The fluidic injection in the nozzle
divergent constitutes an alternative procedure to achieve the goal. In
this paper, we present a 3D analytical model for fluidic injection
in a supersonic nozzle integrating an orifice. The fluidic vectoring
uses a sonic secondary injection in the divergent. As a result, the
flow and interaction between the main and secondary jet has built in
order to express the pressure fields from which the forces and thrust
vectoring are deduced. Under various separation criteria, the present
analytical model results are compared with the existing numerical
and experimental data from the literature.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {9},
	  number    = {7},
	  year      = {2015},
	  pages     = {1352 - 1358},
	  ee        = {https://publications.waset.org/pdf/10002314},
	  url   	= {https://publications.waset.org/vol/103},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 103, 2015},
	}