Publication Date:
2013-08-31
Description:
An experimental Adaptive Wall Test Section (AWTS) process is described. Comparisons of the ONERA T2 and the 0.3-m TCT (transonic cryogenic tunnel) AWTS data for the ONERA CAST-10 airfoil are presented. Most of the 0.3-m TCT data is new and preliminary and no sidewall boundary layer control is involved. No conclusions are given.
Keywords:
AERODYNAMICS
Type:
CAST-10-2(DOA 2 Airfoil Studies Workshop Results; p 137-153
Format:
application/pdf