Datenbestand vom 29. November 2024
Verlag Dr. Hut GmbH Sternstr. 18 80538 München Tel: 0175 / 9263392 Mo - Fr, 9 - 12 Uhr
aktualisiert am 29. November 2024
978-3-8439-3636-1, Reihe Luftfahrt
Jae Hun You Aeroacoustic Characteristics of a Shrouded Helicopter Tail Rotor
224 Seiten, Dissertation Technische Universität München (2017), Softcover, B5
In order to reduce the aerodynamic noise emission from a shrouded tail rotor, an in-depth understanding of flow phenomena associated with the noise generation is necessary. For this purpose, a hybrid method combining unsteady Reynolds-averaged Navier-Stokes simulations with the Ffowcs Williams and Hawkings acoustic analogy is employed. The investigation exemplarily indicates that active flow control via boundary layer suction effectively eliminates the inlet flow distortion, thus reducing the far field noise level by about 5 dB in the forward flight condition.