Numerical and experimental investigation on the effect of a plasma actuator on NLF0414 airfoils' efficiency after the stall
A Salmasi - Modares Mechanical Engineering, 2013 - mme.modares.ac.ir
A Salmasi
Modares Mechanical Engineering, 2013•mme.modares.ac.ir… The purpose of this paper ce of the body force vector indu erically and experimentally for a
N no plasma actuator located o p of the airfoil in order to investigate ma actuator on the top
surfac x=16 mm to x=41 mm at the angle of f lift to drag coefficient or the efficienc … can delay
separation by is to simulate a NLF0414 specific plasma actuator. LF0414 airfoil with the the
airfoil and with body e effect of plasma on the of the airfoil, close to the 18 degrees. This of the …
N no plasma actuator located o p of the airfoil in order to investigate ma actuator on the top
surfac x=16 mm to x=41 mm at the angle of f lift to drag coefficient or the efficienc … can delay
separation by is to simulate a NLF0414 specific plasma actuator. LF0414 airfoil with the the
airfoil and with body e effect of plasma on the of the airfoil, close to the 18 degrees. This of the …
Abstract
Plasma actua inducing external momen airfoil both experimentall For this reason, the sim compressible force produced by a plasm flow passing over it. The separation point separation delay caused a angle of attack.
mme.modares.ac.ir
以上显示的是最相近的搜索结果。 查看全部搜索结果