Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
Book Description
Fuselage Shell and Cavity Response Measurements on a DC-9 Test Section
Fuselage Shell and Cavity Response Measurements on a DC-9 Test Section
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781729353356
Category :
Languages : en
Pages : 60
Book Description
A series of fuselage shell and cavity response measurements conducted on a DC-9 aircraft test section are described. The objectives of these measurements were to define the shell and cavity model characteristics of the fuselage, understand the structural-acoustic coupling characteristics of the fuselage, and measure the response of the fuselage to different types of acoustic and vibration excitation. The fuselage was excited with several combinations of acoustic and mechanical sources using interior and exterior loudspeakers and shakers, and the response to these inputs was measured with arrays of microphones and accelerometers. The data were analyzed to generate spatial plots of the shell acceleration and cabin acoustic pressure field, and corresponding acceleration and pressure wavenumber maps. Analysis and interpretation of the spatial plots and wavenumber maps provided the required information on modal characteristics, structural-acoustic coupling, and fuselage response. Simpson, M. A. and Mathur, G. P. and Cannon, M. R. and Tran, B. N. and Burge, P. L. Unspecified Center...
Publisher: Independently Published
ISBN: 9781729353356
Category :
Languages : en
Pages : 60
Book Description
A series of fuselage shell and cavity response measurements conducted on a DC-9 aircraft test section are described. The objectives of these measurements were to define the shell and cavity model characteristics of the fuselage, understand the structural-acoustic coupling characteristics of the fuselage, and measure the response of the fuselage to different types of acoustic and vibration excitation. The fuselage was excited with several combinations of acoustic and mechanical sources using interior and exterior loudspeakers and shakers, and the response to these inputs was measured with arrays of microphones and accelerometers. The data were analyzed to generate spatial plots of the shell acceleration and cabin acoustic pressure field, and corresponding acceleration and pressure wavenumber maps. Analysis and interpretation of the spatial plots and wavenumber maps provided the required information on modal characteristics, structural-acoustic coupling, and fuselage response. Simpson, M. A. and Mathur, G. P. and Cannon, M. R. and Tran, B. N. and Burge, P. L. Unspecified Center...
Scientific and Technical Aerospace Reports
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 898
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 898
Book Description
Government Reports Announcements & Index
Analysis of Interior Noise Ground and Flight Test Data for Advanced Turboprop Aircraft Applications
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638
Book Description
Smart Structures and Materials
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1142
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1142
Book Description