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Featured researches published by Roland Kube.


Journal of The American Helicopter Society | 1997

Key Results from a Higher Harmonic Control Aeroacoustic Rotor Test (HART)

W.R. Splettstößer; Roland Kube; W. Wagner; U. Seelhorst; A. Boutier; F. Micheli; E. Mercker; Kurt Pengel

In a major cooperative research program within existing US-German and US-French Memoranda of Understandings (MoUs) a comprehensive experimental study was conducted with a 40-percent geometrically and dynamically scaled BO-105 main rotor operated in the open-jet-anechoic test section of the German-Dutch Wind Tunnel (DNW). The objectives of the program were to improve the physical understanding and the mathematical modelling of the effects of the higher harmonic blade pitch control technique on blade-vortex interaction (BVI) impulsive noise and vibration reduction. A unique set of acoustic, dynamic, dynamic response, performance, and rotor wake data were acquired with a pressure and strain gauge instrumentedblade and by application of non-intrusive measurement techniques. This paper is focused on the experimental part of this research program, termed Higher-harmonic-control Aeroacoustic Rotor Test (HART) which was jointly performed by researchers from the.


Journal of The American Helicopter Society | 1994

A Higher Harmonic Control Test in the DNW to Reduce Impulsive BVI Noise

Wolf R. Splettstoesser; Klaus-J. Schultz; Roland Kube; Thomas F. Brooks; Earl R. Booth; Georg Niesl; Olivier Streby

A model rotor acoustic test was performed to examine the benefit of higher-harmonic control (HHC) of blade pitch to reduce blade-vortex interaction (BVI) impulsive noise. A 40-percent dynamically scaled, four-bladed model of a BO-105 main rotor was tested in the German-Dutch Wind Tunnel (DNW). Acoustic measurements were made in a large plane underneath the rotor employing a traversing in-flow microphone array in the anechoic environment of the open test section. Noise characteristics and noise directivity patterns as well as vibratory loads were measured and used to demonstrate the changes when different HHC schedules (different modes, amplitudes, phases) were applied. Dramatic changes of the acoustic signatures and the noise radiation directivity with HHC phase variations were found.


Archive | 1995

Prediction and Measurement of Blade-Vortex Interaction Loading,

Chee Tung; Judith M. Gallman; Roland Kube; Thomas F. Brooks; Gilles Rahier


Journal of Aircraft | 1998

Prediction and Measurement of Blade-Vortex Interaction

Chee Tung; Roland Kube; Thomas F. Brooks; Gilles Rahier


Proc. of AHS/RAcS International Technical Specialists Meeting-Rotorcraft Acoustics and Fluid Dynamics | 1991

HHC Study in the DNW to Reduce BVI Noise - An Analysis

Thomas F. Brooks; Earl R. Booth; Doug Boyd; Wolf R. Splettstoesser; Klaus J. Schultz; Roland Kube; Georg Niesl; Olivier Streby


AHS International Forum 55 | 1999

IBC Effects on BVI Noise and Vibrations - A Combined Numerical and Experimental Investigation

Roland Kube; Deutsches Zentrum f r Luft und Raumfahrt e.V.; B. G. van der Wall; K.-J. Schultz; W.R. Splettstoesser


Archive | 1991

BVI Impulsive Noise Reduction by Higher Harmonic Pitch Control: Results of a Scaled Model Rotor Experiment in the DNW

Wolf R. Splettstoesser; Klaus-J. Schultz; Roland Kube; Thomas F. Brooks; Earl R. Booth; Georg Niesl; Olivier Streby


Archive | 1995

On the Blade Deformation Measured at a Scaled Helicopter Rotor

Edzard Mercker; Kurt Pengel; Roland Kube; Berend G. van der Wall; A. Boutier; F. Micheli


Journal of The American Helicopter Society | 1992

New Aspects of Higher Harmonic Control on a Four-Bladed Hingeless Model Rotor.

Roland Kube


Archive | 1994

Mechanisms of Vibration and BVI Noise Reduction by Higher Harmonic Control

Roland Kube; Berend G. van der Wall; Klaus-J. Schultz

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