Zobrazeno 1 - 10
of 20
pro vyhledávání: '"Sanghyun Chae"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
In this study, ground tests and numerical analysis were performed to verify the hover performance of the second ducted fan model designed by this research team. Shape of the duct inner surface was asymmetric in longitudinal direction, and considering
Externí odkaz:
https://doaj.org/article/d2b1b4af9a3941459decc68586fd7938
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
This work attempts to reduce the hub vibratory loads of a lift-offset rotor using IBC (individual blade pitch control) in high-speed forward flight. As a lift-offset rotor for the present study, the rigid coaxial rotor of a XH-59A compound helicopter
Externí odkaz:
https://doaj.org/article/30eb870cb5664e8f9ec0915c8d473e66
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 49:859-870
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::23f082fb5a4ce25edd296ef4490f41ef
https://doi.org/10.5139/jksas.2021.49.10.859
https://doi.org/10.5139/jksas.2021.49.10.859
Publikováno v:
Lecture Notes in Electrical Engineering ISBN: 9789811926884
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::60566e1f9891620b3baf1b210920a54f
https://doi.org/10.1007/978-981-19-2689-1_36
https://doi.org/10.1007/978-981-19-2689-1_36
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 48:597-609
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b3f10a7dc48bb03fe72b1a9867914583
https://doi.org/10.5139/jksas.2020.48.8.597
https://doi.org/10.5139/jksas.2020.48.8.597
Autor:
Sanghyun Chae, Kim， Deog-Kwan
Publikováno v:
Journal of Computational Fluids Engineering. 25:98-104
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a09abe24011f836cec67e153f8cc8c42
https://doi.org/10.6112/kscfe.2020.25.2.098
https://doi.org/10.6112/kscfe.2020.25.2.098
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 46:41-51
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52b9c501753a5a188746b7d3f9b87e1b
https://doi.org/10.5139/jksas.2018.46.1.41
https://doi.org/10.5139/jksas.2018.46.1.41
Publikováno v:
Journal of the Korean Society of Propulsion Engineers. 21:51-62
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d954da44ec3788280fc0f9e41cac55a1
https://doi.org/10.6108/kspe.2017.21.1.051
https://doi.org/10.6108/kspe.2017.21.1.051
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
This work attempts to reduce the hub vibratory loads of a lift-offset rotor using IBC (individual blade pitch control) in high-speed forward flight. As a lift-offset rotor for the present study, the rigid coaxial rotor of a XH-59A compound helicopter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1c08761891103d55df5f38c2f9820e95
Publikováno v:
AIAA Journal. 54:3546-3563
A modified method has been suggested to improve the computational efficiency of a multiresolution analysis for implicit temporal integrations. The fundamental idea behind multiresolution analysis is that high cost computations such as flux evaluation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::072e914c5c742e6190c5ef323bc39c3f
https://doi.org/10.2514/1.j054644
https://doi.org/10.2514/1.j054644