Publication Date:
2019-08-28
Description:
The experimental results of steady and unsteady pressure measurements, carried out in subsonic and transonic flow on a 16 percent relative thickness supercritical aerofoil, equipped with a trailing edge flap involving 25 percent of the chord, in a sinusoidal motion are given. These experimental results are compared with those obtained by various methods of steady and unsteady inviscid flow calculations. Some calculation results in which viscous effects have been taken into account, for both steady and unsteady flows, are also presented.
Keywords:
AERODYNAMICS
Type:
NASA-TM-75775
,
AGARD-CP-262
Format:
application/pdf
Permalink