Central processor unit times and memory requirements for a commonly used solver are compared to that of a state-of-the-art, parallel, sparse solver. The sparse solver is then used in conjunction with three constrained optimization methodologies to assess the relative merits of non-axisymmetric versus axisymmetric liner concepts for improving liner acoustic suppression. This assessment is performed with a multimodal noise source (with equal mode amplitudes and phases) in a finite-length rectangular duct without flow. The sparse solver is found to reduce memory requirements by a factor of five and central processing time by a factor of eleven when compared with the commonly used solver. Results show that the optimum impedance of the uniform l...
More than ever, there is flexibility and freedom in acoustic liner design. Subject to practical cons...
The current form of the Silent Aircraft is a blended wing design with the propulsion system embedded...
Because communities are impacted by steady increases in aircraft traffic, aircraft noise continues t...
In this paper we demonstrate the usefulness of the ducted fan noise prediction code TBIEM3D as a lin...
An extensive duct acoustics propagation study is presented that has been conducted to assess the des...
The main object of this thesis is to investigate acoustic lining in turbofan ducts which have optima...
In this article the attenuation of broadband noise in an acoustically-lined circular-section duct is...
This thesis contains original research into the propagation of sound in acoustically lined ductswith...
Sound wave propagation in a soft-walled rectangular duct with steady uniform flow was investigated a...
New calculations show that segmenting is most efficient at high frequencies with relatively long duc...
International audienceThe noise radiated at the inlet of turbo-fan engines corresponds to a signific...
Results are presented from detailed analytical studies made to define methods for obtaining improved...
International audienceThe SALUTE project aims at evaluating performance of metacomposites for acoust...
Optimum and off-optimum properties of circumferentially segmented duct liners are compared with thos...
This paper employs three acoustic propagation codes to explore variable-depth liner configurations f...
More than ever, there is flexibility and freedom in acoustic liner design. Subject to practical cons...
The current form of the Silent Aircraft is a blended wing design with the propulsion system embedded...
Because communities are impacted by steady increases in aircraft traffic, aircraft noise continues t...
In this paper we demonstrate the usefulness of the ducted fan noise prediction code TBIEM3D as a lin...
An extensive duct acoustics propagation study is presented that has been conducted to assess the des...
The main object of this thesis is to investigate acoustic lining in turbofan ducts which have optima...
In this article the attenuation of broadband noise in an acoustically-lined circular-section duct is...
This thesis contains original research into the propagation of sound in acoustically lined ductswith...
Sound wave propagation in a soft-walled rectangular duct with steady uniform flow was investigated a...
New calculations show that segmenting is most efficient at high frequencies with relatively long duc...
International audienceThe noise radiated at the inlet of turbo-fan engines corresponds to a signific...
Results are presented from detailed analytical studies made to define methods for obtaining improved...
International audienceThe SALUTE project aims at evaluating performance of metacomposites for acoust...
Optimum and off-optimum properties of circumferentially segmented duct liners are compared with thos...
This paper employs three acoustic propagation codes to explore variable-depth liner configurations f...
More than ever, there is flexibility and freedom in acoustic liner design. Subject to practical cons...
The current form of the Silent Aircraft is a blended wing design with the propulsion system embedded...
Because communities are impacted by steady increases in aircraft traffic, aircraft noise continues t...