Zobrazeno 1 - 10
of 135
pro vyhledávání: '"Louw H"'
Autor:
Louw, H. J.
Publikováno v:
Architectural History, 1987 Jan 01. 30, 45-49.
Externí odkaz:
https://www.jstor.org/stable/1568513
Autor:
Louw, H. J.
Publikováno v:
Architectural History, 1984 Jan 01. 27, 503-509.
Externí odkaz:
https://www.jstor.org/stable/1568491
Autor:
Louw, H. J.
Publikováno v:
Architectural History, 1983 Jan 01. 26, 49-150.
Externí odkaz:
https://www.jstor.org/stable/1568434
Autor:
Louw, H. J.
Publikováno v:
Architectural History, 1981 Jan 01. 24, 1-144.
Externí odkaz:
https://www.jstor.org/stable/1568393
Autor:
Louw, H J
Archaeologia Aeliana, 17, 93-115
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ed6ca6e391b9bfb941a543ed7d76cf4
Autor:
Louw H. van Zyl, Becker van Niekerk
Publikováno v:
2019 16th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
The requirements for modal testing of aircraft structures are not demanding in terms of frequency range, size or weight of sensors, or power required to perform the tests. Yet typical ground vibration test (GVT) systems used for this purpose are expe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b295015711e09d4c5f2a8232b2c79c7
https://doi.org/10.1109/ibcast.2019.8667243
https://doi.org/10.1109/ibcast.2019.8667243
Autor:
Bogaers, Alfred E.J., Oxtoby, Oliver F., Heyns, Johan A., Suliman, Ridhwaan, van Zyl, Louw H.
Publikováno v:
UPCommons. Portal del coneixement obert de la UPC
Universitat Politècnica de Catalunya (UPC)
Universitat Politècnica de Catalunya (UPC)
In this paper, linear and quadratic modal approximations of elastodynamic solid deformation in FSI problems are considered. Firstly, the theory of quadratic exten- sion of modal analysis presented in [1] is laid out. The quadratic and linear approxim
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::f7173df2e6731cb833faec5b8aa323fe
https://hdl.handle.net/2117/190630
https://hdl.handle.net/2117/190630
Publikováno v:
Progress in Aerospace Sciences. 71:54-84
© 2014 Elsevier Ltd.Flutter of T-tail configurations is caused by the aeroelastic coupling between the vertical fin and the horizontal stabiliser. The latter is mounted on the fin instead of the fuselage, and hence the arrangement presents distinct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c7cbb2f4570c46365c3a5f457d9b015
https://doi.org/10.1016/j.paerosci.2014.07.002
https://doi.org/10.1016/j.paerosci.2014.07.002
Publikováno v:
Journal of Aircraft. 51:1805-1812
A fully coupled partitioned fluid–structure interaction technology is developed for transonic aeroelastic structures undergoing nonlinear displacements. The Euler equations, written in an arbitrary Lagrangian–Eulerian coordinate frame, describe t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::33497d31e27bd36ab360884ee0cc1ecb
https://doi.org/10.2514/1.c032524
https://doi.org/10.2514/1.c032524
Autor:
LOUW, H. J.
Publikováno v:
Construction History, 1987 Jan 01. 3, 31-54.
Externí odkaz:
https://www.jstor.org/stable/41613633