Zobrazeno 1 - 10
of 118
pro vyhledávání: '"Soo Hyung Park"'
Autor:
Byambakhand Battumur, Ji Eun Lee, Soo Hyung Park, You-Jung Choi, Dong Oh Kang, Eun Jin Park, Ji Bak Kim, Jah Yeon Choi, Seung Young Roh, Jin Oh Na, Cheol Ung Choi, Jin Won Kim, Seung Woon Rha, Chang Gyu Park, Eung Ju Kim
Publikováno v:
The Korean Journal of Internal Medicine, Vol 38, Iss 4, Pp 514-525 (2023)
Background/Aims Cardiorespiratory fitness (CRF), as measured by maximal oxygen consumption (VO2max), is an important independent predictive factor of cardiovascular outcomes in patients with heart failure (HF). However, it is unclear whether conventi
Externí odkaz:
https://doaj.org/article/4615ea59c84441dfa378a50fc3672b33
Publikováno v:
Aerospace, Vol 11, Iss 2, p 102 (2024)
The air and structural loads of a 5-ton class light helicopter (LH) rotor in a 2.24 g pull-up maneuver are investigated using a coupling between the computational structural dynamics (CSD) and computational fluid dynamics (CFD) methods. The LH rotor
Externí odkaz:
https://doaj.org/article/58a808b76f93487e989225c3bcb0756a
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
The selection of an appropriate turbulence/transition model is critical when simulating the hypersonic flows based on the Reynolds-averaged Navier–Stokes (RANS) equation. In particular, a deep understanding of the validity, reliability, and limitat
Externí odkaz:
https://doaj.org/article/9a2e995c3ecd41649dbc77d7b9e1a59d
Publikováno v:
Applied Sciences, Vol 10, Iss 20, p 7375 (2020)
Many previous studies have shown that wing corrugation of an insect wing is only structurally beneficial in enhancing the wing’s bending stiffness and does not much help to improve the aerodynamic performance of flapping wings. This study uses two-
Externí odkaz:
https://doaj.org/article/e203851b38754172acc158803541f166
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 51:75-84
Autor:
Tae-Hee Kim, Soo-Hyung Park
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 51:85-92
Publikováno v:
Journal of the Korean Society for Aeronautical & Space Sciences. 51:1-8
Publikováno v:
AIAA Journal. 61:355-377
High-order spatial schemes, which effectively treat the dissipative characteristics of computational fluid dynamics solvers, are known to assure the precise prediction of rotorcraft aeroacoustics. However, such schemes may differ in numerical perform
Publikováno v:
AIAA Journal. :1-16
The recent growing interest in urban air mobility (UAM) worldwide has led to the demand for physical analyses of the aerodynamic performance and aeroacoustic characteristics of electric vertical ta...
Publikováno v:
International Journal of Aerospace Engineering. 2021:1-24
The selection of an appropriate turbulence/transition model is critical when simulating the hypersonic flows based on the Reynolds-averaged Navier–Stokes (RANS) equation. In particular, a deep understanding of the validity, reliability, and limitat