Optimizing of the Structural Parameters of an Asymmetric Ramp Micro-Vortex Generator in Supersonic Flow
0
Citation
0
Reference
20
Related Paper
Keywords:
Vortex generator
Choked flow
Cite
Cite
Citations (1)
Cite
Citations (0)
Cite
Citations (2)
Torque converter
Cite
Citations (0)
Cite
Citations (0)
Limit load
Cite
Citations (0)
This study aims to identify aerodynamic characteristics of the ramp tab, a mechanical deflector, by conducting a non-combustive experiment using compressed air and supersonic flow test equipment. With the ramp tabs installed symmetrically and asymmetrically on the outlet of the supersonic nozzle, the structure of the flow field, the thrust spoilage, the thrust deviation angle, and the lift/drag coefficients were derived and analyzed. The results show that the asymmetrically-installed ramp tabs are advantageous relative to the symmetrically-installed tabs in terms of the performance of thrust vector control, thrust deviation angle, and lift coefficient.
Lift (data mining)
Cite
Citations (0)
Cite
Citations (1)
Diffuser (optics)
Cite
Citations (4)