Publication Date:
2019-06-28
Description:
A wind tunnel test of a 16.8 ft. model of a rotor having passively controlled pivotable tips is described. Performance and vibratory hub load data are presented which compare the performance of the rotor with the tips free and fixed. A brief analysis of the experimental findings is included.
Keywords:
AERODYNAMICS
Type:
NASA-CR-166361
,
NAS 1.26:166361
Format:
application/pdf