Zobrazeno 1 - 10 of 17 pro vyhledávání: '"Seung-Kil Paek"'
5
Active Gurney Flap Design Modification for High Speed Operation and Natural Frequency Estimate
Autor: Seung-Kil Paek, Taejoo Kim, Do-Hyung Kim
Publikováno v: Transactions of the Korean Society for Noise and Vibration Engineering. 25:667-676
Working displacement variation by elastic deformation of active Gurney flap which was operated on high frequency was observed. Flap-wise natural frequency was lower than mode analysis result and hinge boundary condition was identified to be the cause
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6a358ba3bf06b620d4c477957d018178
https://doi.org/10.5050/ksnve.2015.25.10.667
Zobrazit plný text záznamu
6
Application and Performance Evaluation of Helicopter Active Vibration Control System for Surion
Autor: Seung-Kil Paek, Taejoo Kim, Do-Hyung Kim, Se-Un Jung, Dong-Il Kwak
Publikováno v: Journal of the Korean Society for Aeronautical & Space Sciences. 43:557-567
The most decisive factor of major sources of a helicopter is the main rotor system and the rotor-induced vibration is one of the technical challenges which should be resolved to ensure comfort for crews and passengers. Passive vibration reduction dev
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4e9bcc7e097fe9ae743e7e41fe9664b5
https://doi.org/10.5139/jksas.2015.43.6.557
Zobrazit plný text záznamu
8
Transonic Nonlinear Aeroelastic Analysis of Aircraft Tail Wings Using Multiblock Approach
Autor: In Lee, Seung Jun Lee, Jong-Yun Kim, Seung-Kil Paek, Kyung-Seok Kim
Publikováno v: Journal of Aircraft. 45:1344-1357
An aeroelastic analysis of a model that uses a combination of horizontal and vertical tails is performed in a transonic flow regime. A transonic small disturbance equation is used for the aerodynamic analysis. The combined model is divided into horiz
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e3c7a3abb70e02f1241ed677f24b23b4
https://doi.org/10.2514/1.34824
Zobrazit plný text záznamu
9
Nonlinear Aeroelastic Instability of a Supersonic Missile Wing. with Pitch Axis Freeplay
Autor: In Lee, Dong-Hyun Kim, Seung-Kil Paek
Publikováno v: International Journal of Aeronautical and Space Sciences. 4:53-62
In this study, nonlinear aeroelastic characteristics of an supersonic missile wing with strong shock interferences are investigated. The missile wing model has a freeplay structural nonlinearity at its pitch axis. To practically consider the effects
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::3cda1c819710f6f081ae89d89f2ed590
https://doi.org/10.5139/ijass.2003.4.1.053
Zobrazit plný text záznamu
10
Transonic/Supersonic Nonlinear Aeroelastic Analysis of a Complete Aircraft Using High Speed Parallel Processing Technique
Autor: Seung-Kil Paek, Hyuk-Jun Kwon, Oh Joon Kwon, Yong-Hee Hyun, Dong-Hyun Kim, In Lee
Publikováno v: Journal of the Korean Society for Aeronautical Space Science. 30:46-55
A nonlinear aeroelastic analysis system in transonic and supersonic flows has been developed using high speed parallel processing technique on the network based PC-clustered machines. This paper includes the coupling of advanced numerical techniques
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5aeb809ac0d2634fc2bfb663fa25f697
https://doi.org/10.5139/jksas.2002.30.8.046
Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání

Omezení vyhledávání
Plný text Recenzováno Digitální knihovna AV ČR
Zdroje