AE-Conference Papers(학술회의논문)

Recent Items

Collection's Items (Sorted by Submit Date in Descending order): 3501 to 3520 of 4783

Vibration Characteristics of Stiffened Laminated Plates Including Thermally Postbuckled Deflection

Lee, Inresearcher; Lee, D.M, 3rd Asian-Pacific Conf. on Computational Mechanics, 1996

Postbuckling and Failure of Stiffened Composite Plates

Hong, Chang Sunresearcher, International Conference on Composite Materials(ICCM), pp.687 - 694, 1997

출력재정의를 통한 비선형제어 기법의 미사일 오톳파일롯 응용

류진훈; 탁민제researcher, 한국자동제어학술회의, 1996-10

BTT missile guidance using neural network

Lee, Y.I.; Sun, B.C.; Lee, H.G.; Tahk, Min-Jearesearcher, 13th World Congress of IFAC, 1996-07

A new design method of unknown input observer

Jin, J.H.; Tahk, Min-Jearesearcher, IFAC Conference on Intelligent Autonomous Control in Aerospace, 1995-08

Optimal guidance for missiles with varying velocity

Cho, H.J.; Ryoo, C.K.; Tahk, Min-Jearesearcher, 34th SICE Annual Conference, 1995-07

Effects of time-to-go freezing on PN guidance loop stability

Rew, D.Y.; Tahk, Min-Jearesearcher, Korea Automatic Control Conference, 1995-10

Application of Multistage Time Stepping Method for 2nd Order Upwind TVD Schemes

Oh, B.S.; Kwon, Jang-Hyukresearcher, Flow Modeling and Turbulence Measurements, pp.141 - 150, 1998

Optimized High-Order Compact Schemes for Linear and Nonlinear Wave Generation and Propagation

Kim, J. W.; Lee, Duck-Jooresearcher, pp.905 - 912, 1996-07

Implementation of Boundary Conditions for the High Order Optimized Compact Schemes

Kim, J. W; Lee, Duck-Jooresearcher, 2nd AIAA/CEAS Aero Acoustic Conference, AIAA, 1996

Third Order Uniformly Non-Oscillatory Schemes with Modified ACM Technique for Linear Wave and Euler Equcation

Lee, Duck-Jooresearcher, AIAA, 1996

A numerical solver for missile/target pursuit-evasion game

Lee, H.G.; Tahk, Min-Jearesearcher, 7th Int. Symp. on Dynamic Games, 1996-12

Postbuckling of Graphite.Epoxy Laminates under Axial Compression

Hong, Chang Sunresearcher, Asian Conference on Computational Mechanics, pp.1585 - 1590, 1996

Three-Dimensional Spiral Vortex Flow past a Bjork-Shiley Valve in an Aorta Using a New Segregated Finite Element Scheme

Chang, Keun Sickresearcher, First Asian CFD Conference, pp.16 - 19, 1995

Impingement of Travelling Shock Wave into a Cavity - A simplified Model for the Hartmann - Sprenger Tube Flow

Chang, Keun Sickresearcher, int. Workshop on Shock Wave/Vortex Interaction, pp.101 - 111, 1997

Adjoint 방법을 이용한 공력최적설계 기법에 관한 연구

성춘호; 권장혁researcher, 한국항공우주학회 춘계학술대회, pp.44 - 48, 한국항공우주학회, 1998

Upwind TVD 기법을 이용한 효율적인 다중격자 DADI 기법

박수형; 성춘호; 권장혁researcher, 한국항공우주학회 춘계학술대회 , pp.71 - 74, 한국항공우주학회, 1998

A New Hyperbolic Equation System with Analysis of Characteristics for Two-phase Flow System

Chang, Keun Sickresearcher, National Heat Transfer Conference, pp.10 - 12, 1997

A Hyperbolic Numerical Method for Two-phase Flows

Chang, Keun Sickresearcher, 2nd International Symposium on Flow Internaction cum Art Lectures/Exhibition, pp.21 - 25, 1997

Three-Dimensional Transonic Airplane Flow Using Unstructured Adaptive Meshes

Chang, Keun Sickresearcher, Second Asian Computational Fluid Dynamics Conference, pp.15 - 18, 1996

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