Recently a ride quality comfort model has been proposed which accounts for the effect of both multifrequency and multiaxes vibratory inputs, as well as nonvibratory inputs such as noise, on human comfort response. The proposed NASA ride quality model is described in general terms and selected results of several experimental investigations are presented that have contributed to the development of the model and to a more comprehensive understanding of human comfort response to vibration. Human subjective response to vertical vibration, combined vertical-lateral vibrations, and roll vibrations are discussed, and a set of vertical discomfort curves is presented
Experimental investigations were conducted to determine the fundamental relationships governing huma...
An experimental investigation was conducted for the combined purposes of determining the relative me...
Two methods of quantifying helicopter ride quality; absorbed power for vibration only and the NASA r...
A model being developed, permits the understanding and prediction of passenger discomfort in a multi...
An extensive research program conducted at NASA Langley Research Center to develop a comprehensive m...
Two of the most important factors, namely, vibration and noise, were studied to (1) determine whethe...
Ride quality vibration criteria applicable to the design and evaluation of air and surface transport...
A simplified empirical model and computer program for estimating passenger ride comfort within air a...
A generalized model was developed for estimating passenger discomfort response to combined noise and...
The results of a simulator study conducted to compare and validate various ride quality prediction m...
The Langley six degree of freedom visual motion simulator has been used to measure subjective respon...
Subjective ride comfort response ratings were measured on the Langley Visual Motion Simulator with v...
Subjective ride comfort response ratings were measured on a visual motion simulator with rolling vel...
An experimental study was conducted to determine the vertical and lateral vibration-transmission cha...
Subjective ride comfort response ratings were measured on the Langley Visual Motion Simulator with l...
Experimental investigations were conducted to determine the fundamental relationships governing huma...
An experimental investigation was conducted for the combined purposes of determining the relative me...
Two methods of quantifying helicopter ride quality; absorbed power for vibration only and the NASA r...
A model being developed, permits the understanding and prediction of passenger discomfort in a multi...
An extensive research program conducted at NASA Langley Research Center to develop a comprehensive m...
Two of the most important factors, namely, vibration and noise, were studied to (1) determine whethe...
Ride quality vibration criteria applicable to the design and evaluation of air and surface transport...
A simplified empirical model and computer program for estimating passenger ride comfort within air a...
A generalized model was developed for estimating passenger discomfort response to combined noise and...
The results of a simulator study conducted to compare and validate various ride quality prediction m...
The Langley six degree of freedom visual motion simulator has been used to measure subjective respon...
Subjective ride comfort response ratings were measured on the Langley Visual Motion Simulator with v...
Subjective ride comfort response ratings were measured on a visual motion simulator with rolling vel...
An experimental study was conducted to determine the vertical and lateral vibration-transmission cha...
Subjective ride comfort response ratings were measured on the Langley Visual Motion Simulator with l...
Experimental investigations were conducted to determine the fundamental relationships governing huma...
An experimental investigation was conducted for the combined purposes of determining the relative me...
Two methods of quantifying helicopter ride quality; absorbed power for vibration only and the NASA r...