Publication Date:
2019-06-27
Description:
Airfoil trailing-edge noise up to a Reynolds number based on chord of 2.96 x 10 to the 6th power was studied. Comparisons are made with current theory, particularly with regard to the nature of the pressure field in the vicinity of the trailing-edge and its influence on the radiated noise.
Keywords:
ACOUSTICS
Type:
NASA-TM-80134
Format:
application/pdf