Zobrazeno 1 - 7
of 7
pro vyhledávání: '"S., Kaitlin"'
Publikováno v:
Journal of Sound and Vibration. 336:240-256
In an effort to model the vibration response of cabled structures, the distributed transfer function method is developed to model cables and a simple cabled structure. The model includes shear effects, tension, and hysteretic damping for modeling of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd9d222e76da1d726385004af21202cc
https://doi.org/10.1016/j.jsv.2014.10.009
https://doi.org/10.1016/j.jsv.2014.10.009
Publikováno v:
Journal of Spacecraft and Rockets. 51:1721-1734
Spaceflight cables are investigated to determine the effect of bakeout on their dynamic response, including resonant frequencies and damping ratios. The addition of cable harnesses to spacecraft structures can affect the dynamic response of the entir
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e78f83b7b336aaddec8a61e2aaf91a0
https://doi.org/10.2514/1.a32780
https://doi.org/10.2514/1.a32780
Publikováno v:
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A cabled beam model is presented in which the cable is modeled as a shear beam attached to an Euler-Bernoulli beam through connections that include both linear and rotational stiffness and damping; the solution is developed through the use of the dis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f29e4767147b38fe36bbb29109c9ec33
https://doi.org/10.2514/6.2015-0690
https://doi.org/10.2514/6.2015-0690
Publikováno v:
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The distributed transfer function method is applied to equations of motion for a space flight cable in an ongoing effort to characterize the effects of adding cabling to space structures. A cable model is presented in which the cable is modeled as a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::574701e6838541abc6779de99558b5fe
https://doi.org/10.2514/6.2014-0491
https://doi.org/10.2514/6.2014-0491
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
In order to develop models for space flight cables, the factors that affect the dynamic response of the cables must be determined. Toward this goal, this work presents the results from a set of experimental tests on 1x18 helically twisted cables made
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b85dc9f22b66e0c26d40f638b07004a
https://doi.org/10.2514/6.2013-1889
https://doi.org/10.2514/6.2013-1889
Akademický článek
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Autor:
G., Jillian, J., Imran, A., Sarita, M., Perla, B., Kevin, S., Kaitlin, V., Katrina, D., Cassadee, H., Haley, C., Spencer, S., Emily
Publikováno v:
Scholastic News: Edition 5/6; 5/5/2008, Vol. 76 Issue 23/24, p15-15, 1p