The paper describes experimental results of an investigation about the propeller vibration and the directivity of sound radiation for some selected resonance frequencies. in an anechoic chamber the spatial distribution of the amplitudes and phase angles of the sound radiation has been measured by means of the reciprocity method. The results indicate that with increasing numbers of propeller blades the spatial variation of the sound amplitude decreases. The origin of the complex nature of the acoustic directivity characteristics in amplitude and phase is the vibration pattern of the propeller. The eigenvalues and the nodal lines of the eigenmodes have been evaluated by holography or by scanning the propeller surface with two acceleration pic...
On the basis of the consideration of various possible kinds of propeller vibrations, the resonance v...
The Near field properties of a 6 " radius model propeller, and the Active Noise Control (ANC) o...
This paper investigates the noise generated by propeller-wing configuration at take-off condition wi...
An experimental program was conducted with the objective of providing high fidelity measurements of ...
The sound field of a rotating propeller is teated theoretically on the basis of aerodynamic principl...
The hydrodynamic and acoustic behavior of a ship propeller is determined by its geometry, load and s...
This paper reports an experimental investigation of noise radiation and psychoacoustic evaluation of...
A study is reported of the influence of non-uniform rotation--which is inherent to piston engine dri...
A theory has been deduced for the "rotation noise" from a propeller with blades of symmetrical secti...
An experimental study was conducted on the noise characteristics of four-bladed general aviation pro...
Propellers usually operate in non-uniform flow conditions, leading to significant levels of noise ge...
International audienceThe present work addresses the scattering of the tonal noise of a low-speed pr...
The present study makes use of microphonic and accelerometric measurement techniques to identify the...
This paper provides a preliminary theoretical investigation of the balance between rotor alone tonal...
Because of recent uncertainty in the price of fuel and also because of concerns over carbon emission...
On the basis of the consideration of various possible kinds of propeller vibrations, the resonance v...
The Near field properties of a 6 " radius model propeller, and the Active Noise Control (ANC) o...
This paper investigates the noise generated by propeller-wing configuration at take-off condition wi...
An experimental program was conducted with the objective of providing high fidelity measurements of ...
The sound field of a rotating propeller is teated theoretically on the basis of aerodynamic principl...
The hydrodynamic and acoustic behavior of a ship propeller is determined by its geometry, load and s...
This paper reports an experimental investigation of noise radiation and psychoacoustic evaluation of...
A study is reported of the influence of non-uniform rotation--which is inherent to piston engine dri...
A theory has been deduced for the "rotation noise" from a propeller with blades of symmetrical secti...
An experimental study was conducted on the noise characteristics of four-bladed general aviation pro...
Propellers usually operate in non-uniform flow conditions, leading to significant levels of noise ge...
International audienceThe present work addresses the scattering of the tonal noise of a low-speed pr...
The present study makes use of microphonic and accelerometric measurement techniques to identify the...
This paper provides a preliminary theoretical investigation of the balance between rotor alone tonal...
Because of recent uncertainty in the price of fuel and also because of concerns over carbon emission...
On the basis of the consideration of various possible kinds of propeller vibrations, the resonance v...
The Near field properties of a 6 " radius model propeller, and the Active Noise Control (ANC) o...
This paper investigates the noise generated by propeller-wing configuration at take-off condition wi...