Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Mihai Mihaila"'
Publikováno v:
INCAS Bulletin, Vol 15, Iss 4, Pp 107-122 (2023)
A study of the air behavior in the near-wake region of the NACA0012 airfoil infinite wing model at low Reynolds numbers was conducted. The study consisted of comparing the results obtained from experiments with those from numerical simulations. The n
Externí odkaz:
https://doaj.org/article/62c7751e0d11491f8c4c63988d803232
Publikováno v:
INCAS Bulletin, Vol 8, Iss 4, Pp 59-65 (2016)
The scope of wing optimization is to design a structure that meets all the airworthiness demands while minimizing its weight. This paper introduces a review for the most important optimization design tools of composite wings with multiple load cases
Externí odkaz:
https://doaj.org/article/dc333c912c204091abc3548a89d7c3a7
Publikováno v:
ACS Applied Energy Materials. 5:7600-7616
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bc267b764619ce59418efbb2bdabfa2
https://doi.org/10.1021/acsaem.2c01059
https://doi.org/10.1021/acsaem.2c01059
Autor:
Vasilica Grigore, Gabriela Alina Paraschiva, Constanta-Valentina Mihaila, Laurentiu Mihai Mihaila
Publikováno v:
Human Systems Management. 40:593-604
BACKGROUND: Finding solutions to increase the efficiency of school organizations is needed in Romanian national education system. In this context, a previous general theoretical approach on school as learning organization (SLO) has been developed bas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0380ac82401eecf12e62741dd750fbd
https://doi.org/10.3233/hsm-201071
https://doi.org/10.3233/hsm-201071
Autor:
Radu Buse, Academia Tehnică Militară, Răzvan Viorel Mihai, Mihai Mihaila-Andres, Radu Calin Pahonie
Publikováno v:
Journal of Military Technology. 1:33-38
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::80192eadeead4337432b1025b71aa119
https://doi.org/10.32754/jmt.2018.1.06
https://doi.org/10.32754/jmt.2018.1.06
Autor:
Radu Calin Pahonie, Ciprian Larco, Carmen Luiza Costuleanu, Cristian Barbu, Vasile Nastasescu, Mihai Mihaila Andres
Publikováno v:
Materiale Plastice. 54:768-772
The paper focuses on the experimental characterization of hyperelastic of the shelf materials in an effort to implement a membrane skin on a low speed asymmetric wing, in order to assess the benefits of flexible lift surfaces. To better determine the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b4e99ca567f80b7a58db888ccbd3922e
https://doi.org/10.37358/mp.17.4.4942
https://doi.org/10.37358/mp.17.4.4942
Autor:
Paul-Virgil Rosu, Mihai Mihaila-Andres, Lucian Constantin, Radu Calin Pahonie, Maria Demsa, Ciprian Larco
Publikováno v:
ITM Web of Conferences, Vol 24, p 02010 (2019)
Nowadays the composite materials have become the materials of choice to be used in the new aerospace structures that need to be not only larger and larger in size but also to be better performing in terms of aeroelastic responses inherent to thin-wal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5aded33ee0d85b7828a2e937f09c4c2d
https://www.itm-conferences.org/articles/itmconf/pdf/2019/01/itmconf_amcse18_02010.pdf
https://www.itm-conferences.org/articles/itmconf/pdf/2019/01/itmconf_amcse18_02010.pdf
Publikováno v:
Review of the Air Force Academy. 13:107-112
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27a64886cdd30df2d20945b72d641591
https://doi.org/10.19062/1842-9238.2015.13.3.18
https://doi.org/10.19062/1842-9238.2015.13.3.18
Publikováno v:
2017 8th International Conference on Mechanical and Aerospace Engineering (ICMAE).
In this paper a new fast preliminary design analysis tool is presented for identifying structural concept models of composite wing structures with emphasize on bend-twist coupling. The research focused on the analysis of a box-beam load carrying stru
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1716e8a097e515805d2a1799dc67d170
https://doi.org/10.1109/icmae.2017.8038669
https://doi.org/10.1109/icmae.2017.8038669
Publikováno v:
AIP Conference Proceedings.
The need of a continuously increasing size and performance of aerospace structures has settled the composite materials as the preferred materials in aircraft structures. Apart from the clear capacity to reduce the structural weight and with it the ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d121211934530bd22cb9c6678955aa63
https://doi.org/10.1063/1.4992590
https://doi.org/10.1063/1.4992590