Wr. Splettstoesser et al., A HIGHER HARMONIC CONTROL TEST IN THE DNW TO REDUCE IMPULSIVE BVI NOISE, Journal of the American Helicopter Society, 39(4), 1994, pp. 3-13
A model rotor acoustic test was performed to examine the benefit of hi
gher harmonic control (HHC) of blade pitch to reduce blade-vortex inte
raction (BVI) impulsive noise. A 40-percent dynamically scaled, four-b
laded model of a BO-105 main rotor was tested in the German-Dutch Wind
Tunnel (DNW). Acoustic measurements were made in a large plane undern
eath the rotor employing a traversing in-flow microphone array in the
anechoic environment of the open test section. Noise characteristics a
nd noise directivity patterns as well as vibratory loads were measured
and used to demonstrate the changes when different HHC schedules (dif
ferent modes, amplitudes, phases) were applied. Dramatic changes of th
e acoustic signatures and the noise radiation directivity with HHC pha
se variations are found. Compared to the baseline conditions (without
HHC), significant mid-frequency noise reductions of as much as 6 dB ar
e obtained for low speed descent conditions where BVI is most intense,
For other rotor operating conditions with less intense BVI there is l
ess or no benefit from the use of HHC. Low frequency loading noise and
vibratory loads, especially at optimum noise reduction control settin
gs, are found to increase.