Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Youngjung Kee"'
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 50:317-323
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5d0d7daaa776ee2d3e69add1048cfc09
https://doi.org/10.5139/jksas.2022.50.5.317
https://doi.org/10.5139/jksas.2022.50.5.317
Publikováno v:
International Journal of Aeronautical and Space Sciences. 21:153-162
This paper proposes a nonlinear finite-element analysis for slender composite structures with anisotropic material properties using the mixed geometrically exact beam formulation and exponential map finite rotation. Rodrigues finite rotation expressi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::047e3956297f8c27929b96252557d416
https://doi.org/10.1007/s42405-019-00207-z
https://doi.org/10.1007/s42405-019-00207-z
Publikováno v:
Journal of the American Helicopter Society. Apr2018, Vol. 63 Issue 2, p1-13. 13p.
Publikováno v:
Journal of Dynamic Systems, Measurement, and Control. 143
A linear quadratic Gaussian (LQG) controller for active vibratory loads reduction in helicopters is proposed based on a revisited higher harmonic control (HHC) input by active trailing-edge flaps (ATEFs). Conventional individual blade control (IBC) i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a91cd3a6ee448e4e76419761521f5a1a
https://doi.org/10.1115/1.4048369
https://doi.org/10.1115/1.4048369
Autor:
JoongYong Park, YoungJung Kee
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 46:159-166
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::524b6fdde0f6c36896fcc9f020c1b9ef
https://doi.org/10.5139/jksas.2018.46.2.159
https://doi.org/10.5139/jksas.2018.46.2.159
Publikováno v:
International Journal of Aeronautical and Space Sciences. 18:641-650
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c614a7736918aad3b524749e75bdf654
https://doi.org/10.5139/ijass.2017.18.4.641
https://doi.org/10.5139/ijass.2017.18.4.641
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 45:581-593
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8536553f44df546093e3322a1b1b963
https://doi.org/10.5139/jksas.2017.45.7.581
https://doi.org/10.5139/jksas.2017.45.7.581
Publikováno v:
Journal of the American Helicopter Society. 61:1-14
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ec31eafc4242f50ab07160dddfcd38a
https://doi.org/10.4050/jahs.61.012005
https://doi.org/10.4050/jahs.61.012005
Publikováno v:
Transactions of the KSME C: Industrial Technology and Innovation. 3:183-191
In this study, the finite element analysis was carried out to investigate dynamic characteristics of the AGF(Active Gurney Flap) which is under development for reducing vibration and noise of the helicopter rotor system. The Gurney flap is a kind of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbf5a0b1eff88f15bde25c08540e3c3c
https://doi.org/10.3795/ksme-c.2015.3.3.183
https://doi.org/10.3795/ksme-c.2015.3.3.183
Publikováno v:
Journal of Dynamic Systems, Measurement, & Control; Jan2021, Vol. 143 Issue 1, p1-12, 12p