Add to ORKGModel problem development and analysis continues with the Alternate Resonance Tuning concept. Various topics are presently at different stages of completion and are described. These topics included optimization of panel mass ratios, panel computer code verification and agreement with experimental data, and flexible frame modeling
Cabin noise in turboprop aircraft causes passenger discomfort, airframe fatigue, and employee schedu...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
A flight and laboratory study of sidewall acoustic treatment for cabin noise control is described. I...
Existing interior noise reduction techniques for aircraft fuselages perform reasonably well at highe...
The reduction of aircraft cabin sound levels to acceptable values still remains a topic of much rese...
Laboratory investigation of sound transmission through panels and the use of modern data analysis te...
Low frequency cabin noise and sonically induced stresses in an aircraft fuselage may be reduced by i...
One of the aims of the EU project FACE (Friendly Aircraft Cabin Environment) is to reduce aircraft i...
Tests were carried out on 20 inch x 20 inch panels at different test conditions using free-free pane...
Noise reduction measurements were made for a simplified model of an airplane fuselage consisting of ...
The noise and vibration in an aircraft cabin during cruise conditions is mostly caused by external f...
Results are presented of full-scale experiments on the active reduction of rotor-induced passenger c...
Analytical and semi-empirical methods for determining the transmission of sound through isolated pan...
Nowadays, the level of interior cabin noise in modern aircraft has been reduced significantly compar...
The generation and control of flight vehicle interior noise is discussed. Emphasis is placed on the ...
Cabin noise in turboprop aircraft causes passenger discomfort, airframe fatigue, and employee schedu...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
A flight and laboratory study of sidewall acoustic treatment for cabin noise control is described. I...
Existing interior noise reduction techniques for aircraft fuselages perform reasonably well at highe...
The reduction of aircraft cabin sound levels to acceptable values still remains a topic of much rese...
Laboratory investigation of sound transmission through panels and the use of modern data analysis te...
Low frequency cabin noise and sonically induced stresses in an aircraft fuselage may be reduced by i...
One of the aims of the EU project FACE (Friendly Aircraft Cabin Environment) is to reduce aircraft i...
Tests were carried out on 20 inch x 20 inch panels at different test conditions using free-free pane...
Noise reduction measurements were made for a simplified model of an airplane fuselage consisting of ...
The noise and vibration in an aircraft cabin during cruise conditions is mostly caused by external f...
Results are presented of full-scale experiments on the active reduction of rotor-induced passenger c...
Analytical and semi-empirical methods for determining the transmission of sound through isolated pan...
Nowadays, the level of interior cabin noise in modern aircraft has been reduced significantly compar...
The generation and control of flight vehicle interior noise is discussed. Emphasis is placed on the ...
Cabin noise in turboprop aircraft causes passenger discomfort, airframe fatigue, and employee schedu...
The design, construction, and costs of a test facility for determining the sound transmission loss c...
A flight and laboratory study of sidewall acoustic treatment for cabin noise control is described. I...