Zobrazeno 1 - 10
of 59
pro vyhledávání: '"Lucas G. Horta"'
Publikováno v:
The Journal of the Astronautical Sciences. 67:335-360
An analytical model is derived to study the structural dynamic stability behavior for the free-flying heliogyro solar sail consisting of a finite set of symmetric or evenly distributed thin blades on a flat surface. Key properties of the flutter inst
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbc1f980d816bc8ec0d8727a4ce78ce6
https://doi.org/10.1007/s40295-019-00153-8
https://doi.org/10.1007/s40295-019-00153-8
Publikováno v:
Model Validation and Uncertainty Quantification, Volume 3 ISBN: 9783030773472
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::438890711955a96564073054a8899f64
https://doi.org/10.1007/978-3-030-77348-9_5
https://doi.org/10.1007/978-3-030-77348-9_5
Autor:
Edmarie Rodríguez Marrero, Axel Figueroa Velez, Andrés Zapata García, Nelson Morales, Michael López Fortún, Elderson Mercado Rivera, Kelby Palencia Torres, Oscar Perales, Gabriel Caro Crespo, Tabatha Maldonado Cardona, Arianna Colon Cesani, Lucas G. Horta, Esmarline de León Peralta, Samuel García León, Wilbert Ruperto, Sofía Rivera Boneta, Giovanni Oliveras Hernandez, María Cortés-Delgado, Fabiola Romero López, Bárbara Calcagño, Agustín Rullán, Aneudy Rodríguez Morales, Derek Quintana Rosa, Pablo Santiago Acevedo, Carlos Catalano Santiago, Gaddiel Gonzalez Mejías, Jonathan Vélez Rivera, Lucas D. Staab, Carla Troche-Vargas, Laury Valentín Rodríguez, Kenneth Colón Rodriguez, Héctor Pérez Ortiz, Jorge Vélez Soto, José Otero Rivera
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ddadda47c98d0305944de7651f18f2f6
https://doi.org/10.2514/6.2019-3882
https://doi.org/10.2514/6.2019-3882
Autor:
Mercedes C. Reaves, Lucas G. Horta
Publikováno v:
International Journal of Crashworthiness. 19:264-274
The paper discusses an application of multi-dimensional calibration metrics to evaluate pressure data from water drop tests of the Max Launch Abort System crew module boilerplate. Specifically, three metrics are discussed: (1) a metric to assess the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d5a07cbf6bf2fdcc7a84d1fb1567942
https://doi.org/10.1080/13588265.2014.883912
https://doi.org/10.1080/13588265.2014.883912
Autor:
Ralph D. Buehrle, Russell A. Parks, Mercedes C. Reaves, Lucas G. Horta, Justin D. Templeton, Paul A. Bartolotta, Daniel R. Lazor, James L. Gaspar
Publikováno v:
Experimental Mechanics. 51:1251-1263
Ares I-X is a flight test vehicle developed by NASA to demonstrate a new class of crew launch vehicle. For this first flight test, the first stage was a four segment solid rocket booster with mass simulators used to represent the other sections of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44af910760407d6c0f3b069449d7a0de
https://doi.org/10.1007/s11340-010-9456-x
https://doi.org/10.1007/s11340-010-9456-x
Publikováno v:
International Journal of Crashworthiness. 15:649-665
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d6ba2e6d741b03a8f88f07484e8b92e
https://doi.org/10.1080/13588265.2010.497020
https://doi.org/10.1080/13588265.2010.497020
Publikováno v:
Journal of the American Helicopter Society. 55:32011-320118
NASA and its contractors are working on structural concepts for absorbing impact energy of aerospace vehicles. Recently, concepts in the form of multi-cell honeycomb-like structures designed to crush under load have been investigated for both space a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e835fc11eb42cfb37a9aa014fa573ce3
https://doi.org/10.4050/jahs.55.032011
https://doi.org/10.4050/jahs.55.032011
Publikováno v:
Computer Methods in Applied Mechanics and Engineering. 197:2607-2620
The objective of this challenge is to develop a data-based probabilistic model of uncertainty to predict the behavior of subsystems (payloads) by themselves and while coupled to a primary (target) system. Although this type of analysis is routinely p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e137730b9573f5087a324099fd1ef5c9
https://doi.org/10.1016/j.cma.2007.07.035
https://doi.org/10.1016/j.cma.2007.07.035
Autor:
Lucas G. Horta, Jiann-Shiun Lew
Publikováno v:
Journal of Sound and Vibration. 308:330-336
In this paper an interval modeling approach for uncertainty quantification of a structure with significant parameter variation is presented. Model uncertainty can be categorized as dominant uncertainty due to structural variation, such as joint uncer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ee4c3bfda1096f1ce4e3eec3e06f839
https://doi.org/10.1016/j.jsv.2007.06.074
https://doi.org/10.1016/j.jsv.2007.06.074
Autor:
Jer-Nan Juang, Samuel C. Gibbs, William K. Wilkie, Karen H. Lyle, Earl H. Dowell, Jay Warren, Dale Lawrence, Lucas G. Horta, Daniel V. Guerrant
Publikováno v:
2nd AIAA Spacecraft Structures Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b70beb2f83dd82c4aa754faaba1211d3
https://doi.org/10.2514/6.2015-0431
https://doi.org/10.2514/6.2015-0431