Topics On Flexible Airplane Dynamics The Application Of Flexible Airframe Transfer Function Approximations And The Sensitivity Of Airframe Transfer Functions To Elastic Mode Shapes
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Topics on Flexible Airplane Dynamics The application of flexible airframe transfer function approximations and the sensitivity of airframe transfer functions to elastic mode shapes
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 62 |
Release | : 1963 |
Genre | : Aeroelasticity |
ISBN | : UOM:39015095304054 |
Download Topics on Flexible Airplane Dynamics The application of flexible airframe transfer function approximations and the sensitivity of airframe transfer functions to elastic mode shapes Book in PDF, Epub and Kindle
pt.3: The dynamic coupling of rigid and elastic degrees of freedom of an airplane are described by two methods. In the first, coupling is described by the changes in airframe characteristic equation roots caused by the introduction of coupling terms to the equations of motion. The second method employs modal response coefficients to compare the relative amplitudes of rigid and elastic degrees of freedom at each coupled mode frequency. Simple literal expressions are obtained for each of these descriptors and physical interpretations given. Time vector diagrams are also used to show the major parameters affecting coupling. (Author).
Scientific and Technical Aerospace Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 300 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : MINN:30000005718667 |
Download Scientific and Technical Aerospace Reports Book in PDF, Epub and Kindle
Topics on Flexible Airplane Dynamics
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 38 |
Release | : 1963 |
Genre | : Aeroelasticity |
ISBN | : UOM:39015095304070 |
Download Topics on Flexible Airplane Dynamics Book in PDF, Epub and Kindle
pt.3: The dynamic coupling of rigid and elastic degrees of freedom of an airplane are described by two methods. In the first, coupling is described by the changes in airframe characteristic equation roots caused by the introduction of coupling terms to the equations of motion. The second method employs modal response coefficients to compare the relative amplitudes of rigid and elastic degrees of freedom at each coupled mode frequency. Simple literal expressions are obtained for each of these descriptors and physical interpretations given. Time vector diagrams are also used to show the major parameters affecting coupling. (Author).
Topics on Flexible Airplane Dynamics Coupling of the rigid and elastic degrees of freedom of an airframe
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 86 |
Release | : 1963 |
Genre | : Aeroelasticity |
ISBN | : UOM:39015095304062 |
Download Topics on Flexible Airplane Dynamics Coupling of the rigid and elastic degrees of freedom of an airframe Book in PDF, Epub and Kindle
pt.3: The dynamic coupling of rigid and elastic degrees of freedom of an airplane are described by two methods. In the first, coupling is described by the changes in airframe characteristic equation roots caused by the introduction of coupling terms to the equations of motion. The second method employs modal response coefficients to compare the relative amplitudes of rigid and elastic degrees of freedom at each coupled mode frequency. Simple literal expressions are obtained for each of these descriptors and physical interpretations given. Time vector diagrams are also used to show the major parameters affecting coupling. (Author).
Topics on Flexible Airplane Dynamics Residual stiffness effects in truncated modal analysis
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 42 |
Release | : 1963 |
Genre | : Aeroelasticity |
ISBN | : UOM:39015095303908 |
Download Topics on Flexible Airplane Dynamics Residual stiffness effects in truncated modal analysis Book in PDF, Epub and Kindle
pt.3: The dynamic coupling of rigid and elastic degrees of freedom of an airplane are described by two methods. In the first, coupling is described by the changes in airframe characteristic equation roots caused by the introduction of coupling terms to the equations of motion. The second method employs modal response coefficients to compare the relative amplitudes of rigid and elastic degrees of freedom at each coupled mode frequency. Simple literal expressions are obtained for each of these descriptors and physical interpretations given. Time vector diagrams are also used to show the major parameters affecting coupling. (Author).
U S Government Research Reports
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 1416 |
Release | : 1964 |
Genre | : Science |
ISBN | : UOM:39015086566430 |
Download U S Government Research Reports Book in PDF, Epub and Kindle
Mitteilungen aus dem Institut f r Flugzeugstatik und Leichtbau an der Eidgen ssischen Technischen Hochschule in Z rich
Author | : Anonim |
Publsiher | : Unknown |
Total Pages | : 152 |
Release | : 1965 |
Genre | : Aeronautics |
ISBN | : UCAL:$B571030 |
Download Mitteilungen aus dem Institut f r Flugzeugstatik und Leichtbau an der Eidgen ssischen Technischen Hochschule in Z rich Book in PDF, Epub and Kindle
Vehicle Design Considerations for Active Control Application to Subsonic Transport Aircraft
Author | : L. Gregor Hofmann,Warren F. Clement |
Publsiher | : Unknown |
Total Pages | : 156 |
Release | : 1974 |
Genre | : Airplanes |
ISBN | : NASA:31769000496110 |
Download Vehicle Design Considerations for Active Control Application to Subsonic Transport Aircraft Book in PDF, Epub and Kindle