Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Carlos Maderuelo"'
Publikováno v:
CEAS Aeronautical Journal. 10:1071-1087
Aeroservoelastic loads calculations usually rely on linear analyses that use implicit structural models (Finite Elements Method) and frequency domain unsteady aerodynamics (Doublet Lattice Method). The hypotheses that underpin this methodology impose
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::56b2993bb66ac27315398bfd43842277
https://doi.org/10.1007/s13272-019-00361-w
https://doi.org/10.1007/s13272-019-00361-w
Autor:
Carmela Rodríguez-Martín, Luis Garcia-Ortiz, Emiliano Rodriguez-Sanchez, Carlos Maderuelo-Fernandez, Alba Lugones-Sanchez, Maria Martin-Cantera, Jose Soriano-Cano, Marta Arietaleanizbeaskoa, Jose Magdalena-Belio, Cristina Menendez-Suarez, Manuel Gómez-Marcos, José Recio-Rodriguez, on behalf of the EVIDENT Investigators EVIDENT Investigators Group
Publikováno v:
Nutrients
Volume 11
Issue 4
Nutrients, Vol 11, Iss 4, p 742 (2019)
Volume 11
Issue 4
Nutrients, Vol 11, Iss 4, p 742 (2019)
Background: Studying the adherence of the population to the Atlantic Diet (AD) could be simplified by an easy and quickly applied dietary index. The aim of this study is to analyse the relationship of an index measuring compliance with recommendation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5c2d6758dbcd2453b084b8423d15b9b1
https://pubmed.ncbi.nlm.nih.gov/30934975
https://pubmed.ncbi.nlm.nih.gov/30934975
Publikováno v:
AIAA Journal. 53:3233-3239
Linear structural dynamics, unsteady aerodynamics, control system, and actuator models are combined for linear aeroservoelastic equations of motion that are augmented with nonlinear feedback loops based on the increased-order modeling approach. Altho
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab397b32a2ae6ea2580ea507d4a492c7
https://doi.org/10.2514/1.j053550
https://doi.org/10.2514/1.j053550
Autor:
Alexander Shousetrman, Mordechay Karpel, Alvaro P. de la Serna, Hector Climent, Carlos Maderuelo
Publikováno v:
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4660ee4334a8635a18b018477dfb3325
https://doi.org/10.2514/6.2013-1702
https://doi.org/10.2514/6.2013-1702
Publikováno v:
49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 16th AIAA/ASME/AHS Adaptive Structures Conference 10t.
A process for calculating dynamic gust loads for structural design of transport aircraft with significant non-linear control-system effects is presented. The process is based on combinations of timeand frequency domain formulations of the equations o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27c53da0fa7b83609decbf86845ef35b
https://doi.org/10.2514/6.2008-1994
https://doi.org/10.2514/6.2008-1994
Publikováno v:
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
Structural design loads in dynamic response to concentrated excitation forces such as in landing and store-ejection impacts are calculated by state-space aeroelastic equations of motion based on the modal approach where the structural displacements a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a1eb06aa7314348aeec298d1c59ae68b
https://doi.org/10.2514/6.2005-2371
https://doi.org/10.2514/6.2005-2371
Publikováno v:
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.
Frequency-domain and time-domain approaches to the calculation of dynamic loads due to response of aeroservoelastic systems to atmospheric gust excitations are presented. The discrete and continuous gust inputs are defined in either time-domain or st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3b1f6667e5aaa63cef6e8c40f336505
https://doi.org/10.2514/6.2004-1592
https://doi.org/10.2514/6.2004-1592
Publikováno v:
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A new modal coupling technique for efficient flutter and aeroservoelastic analyses of aircraft with multiple external-store configurations is presented. The aircraft is represented by a set of free-free normal modes obtained with large fictitious mas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bf3c35e9e59d53c4e76ae54369d3605b
https://doi.org/10.2514/6.2002-1597
https://doi.org/10.2514/6.2002-1597