Add to ORKGThe noise control characteristics of synchrophasing are investigated using a simplified model of an aircraft fuselage. The analysis presented includes directivity effects of the noise sources and solves the coupled motion between the interior and exterior acoustic fields and the shell vibrational response in closed form. The variation in sound pressure level at various locations inside the shell is studied for various synchrophase angles as well as the shell vibrational response and input power flow in order to uncover the principal mechanisms behind the transmission phenomena
Computer codes for predicting noise level inside aircrafts point out some typical frequencies in noi...
"\"An integrated spectral-integral formulation is applied for prediction and active control of. the ...
Active control of sound transmitted through an elastic panel when excited by a turbulent boundary la...
A simplified cylindrical model of an aircraft fuselage is used to investigate the mechanisms of inte...
The noise control characteristics of synchrophasing are investigated using a simplified model of an ...
Blacksburg, V i r g i n i a 24061 v I n t h i s paper the noise cont ro l character is-t i c s of sy...
This thesis provides a new and detailed examination of how the optimum propeller synchrophase angles...
Experimental determination of the sound insulation of propfan aircraft fuselage structures is proble...
A simplified cylindrical model of an aircraft fuselage is used to investigate the mechanisms of inte...
A light aircraft fuselage was modeled as a half-scale cylindrical shell to study the sound transmiss...
In this paper, the theory and the results are presented of a study concerned with the active control...
"August 1984"--Cover.Subject category 71.Distributed to depository libraries in microfiche."Virginia...
It is very important to predict the acoustic behavior of the fuselage cabin for the noise control. S...
The sound transmission loss of lightweight structures can be increased by the application of facing ...
The following report deals in preliminary fashion with the transmission through a fuselage of random...
Computer codes for predicting noise level inside aircrafts point out some typical frequencies in noi...
"\"An integrated spectral-integral formulation is applied for prediction and active control of. the ...
Active control of sound transmitted through an elastic panel when excited by a turbulent boundary la...
A simplified cylindrical model of an aircraft fuselage is used to investigate the mechanisms of inte...
The noise control characteristics of synchrophasing are investigated using a simplified model of an ...
Blacksburg, V i r g i n i a 24061 v I n t h i s paper the noise cont ro l character is-t i c s of sy...
This thesis provides a new and detailed examination of how the optimum propeller synchrophase angles...
Experimental determination of the sound insulation of propfan aircraft fuselage structures is proble...
A simplified cylindrical model of an aircraft fuselage is used to investigate the mechanisms of inte...
A light aircraft fuselage was modeled as a half-scale cylindrical shell to study the sound transmiss...
In this paper, the theory and the results are presented of a study concerned with the active control...
"August 1984"--Cover.Subject category 71.Distributed to depository libraries in microfiche."Virginia...
It is very important to predict the acoustic behavior of the fuselage cabin for the noise control. S...
The sound transmission loss of lightweight structures can be increased by the application of facing ...
The following report deals in preliminary fashion with the transmission through a fuselage of random...
Computer codes for predicting noise level inside aircrafts point out some typical frequencies in noi...
"\"An integrated spectral-integral formulation is applied for prediction and active control of. the ...
Active control of sound transmitted through an elastic panel when excited by a turbulent boundary la...