Browse "AE-Conference Papers(학술회의논문)" by Title 

Showing results 2236 to 2255 of 5212

2236
Pairing Asymmetry-induced Collective Dynamics of Lean-premixed Model Gas Turbine Combustors

Bae, Dahyun; Kim, Kyu Tae, The 19th International Conference on Flow Dynamics, ICFD2022, Institute of Fluid Science, 2022-11-11

2237
PANS를 이용한 벽면에 붙어있는 정육면체 주변의 유동장 해석

송지수; 박승오, 2007년도 한국군사과학기술학회 종합학술대회, 2007-08-17

2238
Parabolized Stability Equation을 이용한 압축성 경계층의 안정성 해석

박동훈; 박승오, 한국항공우주학회 학술발표회, pp.204 - 208, 한국항공우주학회, 2008-11

2239
Parallel Performance Assessment of Moving Body Overset Grid Application on PC Cluster

Kim, E.; Kwon, Jang-Hyuk; Park, S.H., PARALLEL COMPUTATIONAL FLUID DYNAMICS, v.18, pp.59 - 66, Amsterdam; Oxford; Elsevier, 2006-05

2240
Parallelization of a Compressible Flow Solver Using Unstructured Grids with Cell-Centered Finite Volume Discretization

Kim, Sung Ho; Kwon, Jang-Hyuk, KSME-JSME Fluids Engineering Conference, pp.769 - 772, 1998

2241
Parameter estimation of rotorcraft using UKF algorithm

Na, C.J.; Hong, J.S.; Bang, Hyochoong, JSASS-KSAS Joint International Symposium on Aerospace Engineering, JSASS, 2005-10-12

2242
Parameter optimization of multistage missile for terminal velocity maximization

Lee, Jun-Yong; Hong, Seong-Min; Kim, Young-Won; Tahk, Min-Jea, 7th Asia-Pacific International Symposium on Aerospace Technology, APISAT 2015, pp.276 - 282, Asia-Pacific International Symposium on Aerospace Technology (APISAT), 2015-11

2243
Parameter Optimization-Based Automatic Design of Launch Vehicle's Attitude Controller

Jung, Ki-Wook; Lee, Chang-Hun, 74th International Astronautical Congress, International Astronautical Federation, 2023-10-04

2244
Parameter Study of Low Noise CROR System

Yi, Seulgi; Kwon, Hyung Il; Choi, Seongim; Park, Min Jun; Lee, Duck Joo, AIAA Aviation 2016, AIAA, 2016-06-15

2245
Parameter Tuning of Linear Active Disturbance Rejection Controller for Altitude Based on Particle Swarm Optimization

Liao, Jingxian; Bang, Hyochoong, 21st International Conference on Control, Automation and Systems, ICCAS 2021, pp.1418 - 1423, IEEE Computer Society, 2021-10

2246
Parameter-robust control design using co-evolution

Hur, J.; Tahk, Min-Jea, JSASS Aircraft Symposium, JSASS, 1998-10

2247
Parametric investigation on plasma streamwise vortex generators with flow around a bluff body

Yoon, Jaesan; Han, Jae Hung, 2015 AIAA Science and Technology Forum and Exposition, American Institute of Aeronautics and Astronautics (AIAA), 2015-01-05

2248
Parametric investigation on the effects of plasma streamwise vortex generators on the flow around a bluff body

Yoon, Jae-San; Han, Jae-Hung, 53rd AIAA Aerospace Sciences Meeting, 2015, American Institute of Aeronautics and Astronautics Inc, AIAA, 2015-01

2249
Parametric Study of a Rapidly Deploying Spoiler with Two-Equation Turbulence Models

Chang, Keun Sick, AIAA General Science Meeting, 2001

2250
Parametric Study of Laser Generated Pulse-Echo Ultrasonic Wave for Nondestructive Testing Applications

Abetew, Ayalsew Dagnew; Hong, Seungchan; Lee, Jung Ryul; Ihn, Jeong Beom, 2016년 한국비파괴검사학회 추계학술대회, 한국비파괴검사학회, 2016-11

2251
Parity space를 이용한 고장진단

진재현; 탁민제, '95 한국항공우주학회 춘계학술발표회, 한국항공우주학회, 1995-04

2252
Partial agreement task assignment algorithm for secure plan consensus in multi-agent system

Kim, Ho-Yeon; Choi, Han-Lim, 18th International Conference on Control, Automation and Systems (ICCAS), pp.856 - 861, IEEE, 2018-10-20

2253
Partial replanning for decentralized dynamic task allocation

Buckman, Noam; How, Jonathan P; Choi, Han-Lim, AIAA Scitech Forum, 2019, American Institute of Aeronautics and Astronautics Inc, AIAA, 2019-01

2254
Particle swarm optimization for airship controller design

Park, C.S.; Bang, Hyochoong; Tahk, Min-Jea, 16th JSASS Aircraft Symposium, pp.137 - 140, JSASS, 2002-10

2255
Pass rate analysis of interception heuristic against border crossers along a linear border

Jang, Dae-Sung; Choi, Han-Lim, International Conference on Control, Automation, Robotics, and Vision, Nanyang Technological University, 2012-12

rss_1.0 rss_2.0 atom_1.0