dc.contributor.author |
Van Zyl, Louwrens H
|
|
dc.date.accessioned |
2008-05-08T07:58:39Z |
|
dc.date.available |
2008-05-08T07:58:39Z |
|
dc.date.issued |
1993-07 |
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dc.identifier.citation |
Van Zyl, L.H. 1993. Use of eigenvectors in the solution of the flutter equation. Journal of Aircraft, Vol. 30(4), pp 553-554 |
en |
dc.identifier.issn |
0021-8669 |
|
dc.identifier.uri |
http://hdl.handle.net/10204/2244
|
|
dc.description.abstract |
The use of eigenvectors to assign eigenvalues to modes for the p-k formulation of the flutter equation is described. The procedure has the potential to overcome some of the problems of the determinant iteration procedure to solve the flutter equation. Advantages of the proposed procedure include the possibility of using a general eigenvalue routine capable of solving repeated eigenvalues, effective distinguishing of eigenvalues, initial frequency values requirement used only for the first calculation of reduced frequency at each speed, and reduced computation time. |
en |
dc.language.iso |
en |
en |
dc.publisher |
American Institute of Aeronautics and Astronautics |
en |
dc.subject |
Aeroelasticity |
en |
dc.subject |
Eigenvectors |
en |
dc.subject |
Flutter |
en |
dc.subject |
Eigenvalues |
en |
dc.subject |
Iterative solution |
en |
dc.subject |
Vibration tests |
en |
dc.subject |
Wings |
en |
dc.title |
Use of eigenvectors in the solution of the flutter equation |
en |
dc.type |
Article |
en |
dc.identifier.apacitation |
Van Zyl, L. H. (1993). Use of eigenvectors in the solution of the flutter equation. http://hdl.handle.net/10204/2244 |
en_ZA |
dc.identifier.chicagocitation |
Van Zyl, Louwrens H "Use of eigenvectors in the solution of the flutter equation." (1993) http://hdl.handle.net/10204/2244 |
en_ZA |
dc.identifier.vancouvercitation |
Van Zyl LH. Use of eigenvectors in the solution of the flutter equation. 1993; http://hdl.handle.net/10204/2244. |
en_ZA |
dc.identifier.ris |
TY - Article
AU - Van Zyl, Louwrens H
AB - The use of eigenvectors to assign eigenvalues to modes for the p-k formulation of the flutter equation is described. The procedure has the potential to overcome some of the problems of the determinant iteration procedure to solve the flutter equation. Advantages of the proposed procedure include the possibility of using a general eigenvalue routine capable of solving repeated eigenvalues, effective distinguishing of eigenvalues, initial frequency values requirement used only for the first calculation of reduced frequency at each speed, and reduced computation time.
DA - 1993-07
DB - ResearchSpace
DP - CSIR
KW - Aeroelasticity
KW - Eigenvectors
KW - Flutter
KW - Eigenvalues
KW - Iterative solution
KW - Vibration tests
KW - Wings
LK - https://researchspace.csir.co.za
PY - 1993
SM - 0021-8669
T1 - Use of eigenvectors in the solution of the flutter equation
TI - Use of eigenvectors in the solution of the flutter equation
UR - http://hdl.handle.net/10204/2244
ER -
|
en_ZA |