Author: Jack D. Leatherwood
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 52
Book Description
Evaluation of Ride Quality Prediction Methods for Helicopter Interior Noise and Vibration Environments
Author: Jack D. Leatherwood
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 52
Book Description
Evaluation of Ride Quality Prediction Methods for Helicopter Interior Noise and Vibration Environments
Author: J. D. Leatherwood
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 52
Book Description
This paper presents the results of a simulator study conducted to compare and validate various ride quality prediction methods for use in assessing passenger/crew ride comfort within helicopters. Included are results quantifying 35 helicopter pilots' discomfort responses to helicopter interior noise and vibration typical of routine flights, assessment of various ride quality metrics including the NASA ride comfort model, and examination of possible criteria approaches. Results of the study indicated that crew discomfort results from a complex interaction between vibration and interior noise. Overall measures such as weighted or unweighted root-mean-square acceleration level and A-weighted noise level were not good predictors of discomfort. Accurate prediction required a metric incorporating the interactive efefcts of both noise and vibration. The best metric for predicting crew comfort to the combined noise and vibration environment was the NASA discomfort index. (Author).
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 52
Book Description
This paper presents the results of a simulator study conducted to compare and validate various ride quality prediction methods for use in assessing passenger/crew ride comfort within helicopters. Included are results quantifying 35 helicopter pilots' discomfort responses to helicopter interior noise and vibration typical of routine flights, assessment of various ride quality metrics including the NASA ride comfort model, and examination of possible criteria approaches. Results of the study indicated that crew discomfort results from a complex interaction between vibration and interior noise. Overall measures such as weighted or unweighted root-mean-square acceleration level and A-weighted noise level were not good predictors of discomfort. Accurate prediction required a metric incorporating the interactive efefcts of both noise and vibration. The best metric for predicting crew comfort to the combined noise and vibration environment was the NASA discomfort index. (Author).
NASA Technical Paper
NASA Reference Publication
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Aeroacoustics of Flight Vehicles: Noise control
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 452
Book Description
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 452
Book Description
Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1984
NASA Scientific and Technical Publications
Aeroacoustics of Flight Vehicles
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 456
Book Description
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 456
Book Description