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Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load


Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load
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Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load


Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load
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Author : Robert W. Hess
language : en
Publisher:
Release Date : 1970

Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load written by Robert W. Hess and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Damping (Mechanics) categories.


The flutter of 13 panels subject to streamwise inplane load at Mach numbers of 1.57 and 1.96 has been investigated. Panel length-width ratios ranged from 1 to 4.2. The experimental flutter boundary was compared with an analytical flutter boundary for six of the panels. Damping, both aerodynamic and structural, was found to have a pronounced effect on the analytical flutter boundary. The agreement between analysis and experiment was dependent upon how structural damping was introduced in the formulation of the problem.



Nasa Technical Report


Nasa Technical Report
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Author :
language : en
Publisher:
Release Date : 1970

Nasa Technical Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aerodynamics categories.




Thermoelastic Damping And Its Effect On Flutter Of Stressed Panels Situated In A Supersonic Airflow


Thermoelastic Damping And Its Effect On Flutter Of Stressed Panels Situated In A Supersonic Airflow
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Author : R. C. Shieh
language : en
Publisher:
Release Date : 1971

Thermoelastic Damping And Its Effect On Flutter Of Stressed Panels Situated In A Supersonic Airflow written by R. C. Shieh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aerodynamics, Supersonic categories.


The effects of material damping on flutter of stressed rectangular panels are studied within the context of linear thermoelasticity theory. The closed-form expression for the thermoelastic (material) damping coefficient is obtained as a function of frequency, panel temperature and dimensions, and material properties. The solution of the stability boundary-value problem is obtained by use of a generalized Galerkin method in the cross-stream direction which reduces the governing partial differential equations to a system of ordinary differential equations in the streamwise direction. These equations are then solved exactly. Numerical results are given for the thermoelastic damping coefficients and for the flutter speeds of partially and fully clamped panels subjected to midplane stress.



Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1970

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Aeronautics categories.




Monthly Catalog Of United States Government Publications Cumulative Index


Monthly Catalog Of United States Government Publications Cumulative Index
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Author : United States. Superintendent of Documents
language : en
Publisher:
Release Date : 1979

Monthly Catalog Of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with United States categories.




Nasa Technical Note


Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1975

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.




A Compilation Of Research Reports Of Physical Research Division Dynamic Loads Division Loads Division 1921 1973


A Compilation Of Research Reports Of Physical Research Division Dynamic Loads Division Loads Division 1921 1973
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Author : Gloria R. Champine
language : en
Publisher:
Release Date : 1977

A Compilation Of Research Reports Of Physical Research Division Dynamic Loads Division Loads Division 1921 1973 written by Gloria R. Champine and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aeronautics categories.




Monthly Catalogue United States Public Documents


Monthly Catalogue United States Public Documents
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Author :
language : en
Publisher:
Release Date : 1970

Monthly Catalogue United States Public Documents written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Government publications categories.




Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load


Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load
DOWNLOAD
Author : Robert W. Hess
language : en
Publisher:
Release Date : 1970

Experimental And Analytical Investigation Of The Flutter Of Flat Built Up Panels Under Streamwise Inplane Load written by Robert W. Hess and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with Damping (Mechanics) categories.


The flutter of 13 panels subject to streamwise inplane load at Mach numbers of 1.57 and 1.96 has been investigated. Panel length-width ratios ranged from 1 to 4.2. The experimental flutter boundary was compared with an analytical flutter boundary for six of the panels. Damping, both aerodynamic and structural, was found to have a pronounced effect on the analytical flutter boundary. The agreement between analysis and experiment was dependent upon how structural damping was introduced in the formulation of the problem.



Aeroelasticity Of Plates And Shells


Aeroelasticity Of Plates And Shells
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Author : E.H. Dowell
language : en
Publisher: Springer Science & Business Media
Release Date : 1974-11-30

Aeroelasticity Of Plates And Shells written by E.H. Dowell and has been published by Springer Science & Business Media this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974-11-30 with Science categories.