Zobrazeno 1 - 10
of 32
pro vyhledávání: '"Giulio Romeo"'
Publikováno v:
Aerospace, Vol 7, Iss 2, p 17 (2020)
CubeSats usually adopt aluminum alloys for primary structures, and a number of studies exist on Carbon Fiber Reinforced Plastic (CFRP) primary structures. The internal volume of a spacecraft is usually occupied by battery arrays, reducing the volume
Externí odkaz:
https://doaj.org/article/66684de85cc94bb6bab0a4dc021520e5
Publikováno v:
Aerospace Science and Technology. 54:1-9
A procedure for the characterization of low velocity impact damage and its effect on residual tensile and buckling behaviour of composite structures is presented. A simplified analytical method is used to enhance the damage simulation and a degradati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4f0cfceed3b1807cb0b5f55855b971c6
https://doi.org/10.1016/j.ast.2016.04.001
https://doi.org/10.1016/j.ast.2016.04.001
Publikováno v:
Aerospace
Volume 7
Issue 2
Aerospace, Vol 7, Iss 2, p 17 (2020)
Volume 7
Issue 2
Aerospace, Vol 7, Iss 2, p 17 (2020)
CubeSats usually adopt aluminum alloys for primary structures, and a number of studies exist on Carbon Fiber Reinforced Plastic (CFRP) primary structures. The internal volume of a spacecraft is usually occupied by battery arrays, reducing the volume
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7e0c6edeb61e6bca39cbdf5a214e109e
https://doi.org/10.3390/aerospace7020017
https://doi.org/10.3390/aerospace7020017
Purpose This paper aims to present a systematic performance-oriented procedure to predict structural responses of composite layered structures. The procedure has a direct application in the preliminary design of aerospace composite structures evaluat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fe9eb9365f0579a4c4e02de5be0ab023
http://hdl.handle.net/11583/2674865
http://hdl.handle.net/11583/2674865
Publikováno v:
MATEC Web of Conferences, Vol 304, p 07001 (2019)
CubeSats primary structures are usually made with aluminium alloys, with few examples of CFRP primary structures under study. Power system battery arrays usually occupy spacecraft internal volume and mass that should be available to the payload. A CF
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::aa1e5f93a43eb60f4d225b4608daad4f
https://doi.org/10.1051/matecconf/201930407001
https://doi.org/10.1051/matecconf/201930407001
Publikováno v:
Journal of Aerospace Engineering. 25:356-368
The application of fuel cell (FC) technology to aircraft propulsion and/or energy supply is becoming of great interest for undoubted advantages in terms of pollution emissions and noise reduction. A better understanding of problems related to fuel ce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::073610c9a6c8f0c3874c8fc22799a7a2
https://doi.org/10.1061/(asce)as.1943-5525.0000138
https://doi.org/10.1061/(asce)as.1943-5525.0000138
Publikováno v:
Journal of Aerospace Engineering. 24:79-88
The application of fuel-cell technology to aircraft propulsion and/or energy supply is becoming of great interest for undoubted advantages in terms of pollution emissions and noise, features particularly important for commuter airplanes that usually
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3f0eb553371f0f39c9e875518770ef88
https://doi.org/10.1061/(asce)as.1943-5525.0000055
https://doi.org/10.1061/(asce)as.1943-5525.0000055
Autor:
Giacomo Frulla, Giulio Romeo
Publikováno v:
Composites Part B: Engineering. 39:656-664
In the study of specific aerospace systems, such as Solar Powered HALE-UAV, the required large structural dimensions force designers to consider modular constructions with removable connections. A specific advanced pin-hole connection has been design
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1f7e67fa325a96cf596d05e70ba8378f
https://doi.org/10.1016/j.compositesb.2007.06.003
https://doi.org/10.1016/j.compositesb.2007.06.003
Publikováno v:
Journal of Guidance, Control, and Dynamics. 30:713-721
This paper addresses stability analysis, control design, and simulation of high-altitude, long-endurance unmanned aerial vehicles. These aircraft are highly flexible and have very low structural frequencies. Hence, the separation between the elastic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1648018a0d4b98f0efeebd76f4f54d91
https://doi.org/10.2514/1.25814
https://doi.org/10.2514/1.25814
The application of fuel cell technology to aircraft propulsion and/or energy supply is attracting a great deal of interest because of the undoubted advantages that can be attained in terms of pollution emissions and noise reduction. The goal of the E
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1565d37cd2827fc0b0138f9963485022
http://journals.sagepub.com/doi/abs/10.1177/0954410014541081
http://journals.sagepub.com/doi/abs/10.1177/0954410014541081