Rotational Axisymmetric Mean Flow for the Vortex Injection Hybrid Rocket Engine

Joseph Majdalani, Anand Vyas
2004 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit   unpublished
Subscripts i = inlet property at the base, z L = r = radial component or partial derivative w = property along the circumferential wall z = axial component or partial derivative D 40th AIAA/ASME/SAE/
doi:10.2514/6.2004-3475 fatcat:2c45hlniofhh5if3fn5g326jsm