Subsonic to Supersonic Wake Stabilization Using Discrete Porosity

The feasibility of using discrete suction to improve the laser optics environment associated with a hemisphere-and-cylinder turret was investigated using computational fluid dynamics. Simulations were conducted at Mach numbers of 0.5, 0.7, and 1.5. The discrete suction control generates and position...

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Veröffentlicht in:	Journal of aircraft 2014-01, Vol.51 (1), p.37-46
Hauptverfasser:	Ng, T. Terry, Patil, S. K. R
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace engineering Aircraft Bandwidths Beams (radiation) Computational fluid dynamics Computer simulation Density Design Downwash Fluid dynamics Lasers Mach number Optics Porosity Propagation Suction Vortices Wakes
Online-Zugang:	Volltext
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