On the role of prediction tools for adaptive rotor system developments

Smart Materials and Structures

Volumn 10, Issue 1, 2001, Pages 137-144

  Kube, R ^a   Kloppel V ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b EUROCOPTER DEUTSCHLAND GMBH   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC VARIABLES CONTROL; ACTUATORS; ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; NAVIER STOKES EQUATIONS; PIEZOELECTRIC DEVICES; TURBOMACHINE BLADES; VIBRATION CONTROL; WIND TUNNELS;

ADAPTIVE ROTOR SYSTEMS; HELICOPTER ENVELOPE; NOISE EMISSION; NOSE DROOP; ROTOR INDUCED VIBRATIONS;

HELICOPTER ROTORS;

EID: 0342420576     PISSN: 09641726     EISSN: None     Source Type: Journal    
DOI: 10.1088/0964-1726/10/1/313     Document Type: Article

References (13)

1. Kube R and Schultz K-J 1996 Vibration and BVI noise reduction by active rotor control: HHC compared to IBC Proc. 22nd Eur. Rotorcraft Forum (Brighton, UK, 1996)
2. Myrtle T F, Friedmann P P and de Terlizzi M 1998 New developments in vibration reduction with actively controlled trailing edge flaps Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
3. Chopra I 1993 Development of a smart rotor Proc. 19th Eur. Rotorcraft Forum (Como, Italy, 1993)
4. Straub F K 1998 Active flap control for vibration reduction and performance improvement Proc. 51st Ann. Forum of the American Helicopter Society (Washington, DC, 1998)
5. Geissler W 1993 Dynamic stall control by airfoil deformation Proc. 19th Eur. Rotorcraft Forum (Como, Italy, 1993)
6. Büter A 1997 Calculations and experimental results of the adaptive twist control concept to reduce helicopter vibrations and noise emissions Proc. Innovation in Rotorcraft Technology (London, UK, 1997)
7. Schimke D, Jänker P, Wendt V and Junker B 1998 Wind tunnel evaluation of a full scale piezoelectric flap control unit Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
8. Raffel M, Dewhirst T, Bretthauer B and Vollmers H 1998 Advanced flow velocity field metrology and their application to helicopter aerodynamics Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
9. Geissler W, Sobieczky H and Vollmers H 1998 Numerical study of the unsteady flow on a pitching airfoil with oscillating flap Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
10. Schultz K-J, Lohmann D, Lieser J A and Pahlke K D 1994 Aeroacoustic calculation of helicopter rotors at DLR Proc. 75th AGARD Fluid Dynamics Symp. (Berlin, Germany, 1994)
11. Splettstoesser W R, Schultz K J, van der Wall B, Buchholz H, Gembler W and Niesl G 1998 The effect of individual blade pitch control on BVI noise - comparison of flight test and simulation results Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
12. Honert H, van der Wall B, Fritzsche M and Niesl G 1998 Realtime BVI noise identification from blade pressure data Proc. 24th Eur. Rotorcraft Forum (Marseille, France, 1998)
13. Schimke D, Kube R and Arnold U T P 1998 Individual blade root control demonstration evaluation of recent flight tests Proc. 54th Ann. Forum of the American Helicopter Society (Washington, DC, 1998)