AE-Journal Papers(저널논문)

Recent Items

Collection's Items (Sorted by Submit Date in Descending order): 3321 to 3340 of 3445

3321
STATIC AEROELASTIC ANALYSIS FOR GENERIC CONFIGURATION WING

Lee, In; MIURA, H; CHARGIN, MK, JOURNAL OF AIRCRAFT, v.28, no.12, pp.801 - 802, 1991-12

3322
STATIC AEROELASTIC CHARACTERISTICS OF A COMPOSITE WING

Lee, In; KIM, SH; MIURA, H, JOURNAL OF AIRCRAFT, v.31, no.6, pp.1413 - 1416, 1994

3323
FINITE-ELEMENT ANALYSIS OF COMPOSITE PANEL FLUTTER

Lee, In; CHO, MH, COMPUTERS STRUCTURES, v.39, no.1-2, pp.165 - 172, 1991

3324
AEROELASTIC STABILITY OF HINGELESS ROTOR BLADE IN HOVER USING LARGE DEFLECTION THEORY

CHO, MH; Lee, In, AIAA JOURNAL, v.32, no.7, pp.1472 - 1477, 1994-07

3325
Refined aeroelastic analysis of hingeless rotor blades in hover

Cho, MH; Jeon, SM; Woo, SH; Lee, In, JOURNAL OF AIRCRAFT, v.34, no.3, pp.408 - 415, 1997

3326
STATIC AND DYNAMIC ANALYSIS OF COMPOSITE BOX BEAMS USING LARGE DEFLECTION THEORY

JEON, SM; CHO, MH; Lee, In, COMPUTERS STRUCTURES, v.57, no.4, pp.635 - 642, 1995-11

3327
Aeroelastic analysis for flap of airfoil in transonic flow

Yang, S; Lee, In, COMPUTERS STRUCTURES, v.61, no.3, pp.421 - 430, 1996-11

3328
Flutter analysis for control surface of launch vehicle with dynamic stiffness

Paek, SK; Lee, In, COMPUTERS STRUCTURES, v.60, no.4, pp.593 - 599, 1996-06

3329
Supersonic flutter analysis of stiffened isotropic and anisotropic panels

Lee, DM; Lee, In, AIAA JOURNAL, v.34, no.3, pp.637 - 639, 1996-03

3330
Aeroelastic analysis of a flexible airfoil with a freeplay non-linearity

Kim, SH; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.193, no.4, pp.823 - 846, 1996-06

3331
Vibration analysis of stiffened laminated plates including thermally postbuckled deflection effect

Lee, DM; Lee, In, JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, v.16, no.12, pp.1138 - 1154, 1997

3332
VIBRATION ANALYSIS OF ANISOTROPIC PLATES WITH ECCENTRIC STIFFENERS

LEE, DM; Lee, In, COMPUTERS STRUCTURES, v.57, no.1, pp.99 - 105, 1995-10

3333
AEROELASTIC ANALYSIS OF MULTIBLADED HINGELESS ROTORS IN HOVER

CHO, MH; Lee, In, AIAA JOURNAL, v.33, no.12, pp.2348 - 2353, 1995-12

3334
Vibration behaviors of thermally postbuckled anisotropic plates using first-order shear deformable plate theory

Lee, DM; Lee, In, COMPUTERS STRUCTURES, v.63, no.3, pp.371 - 378, 1997-05

3335
AEROELASTIC ANALYSIS OF A FLEXIBLE CONTROL SURFACE WITH STRUCTURAL NONLINEARITY

Lee, In; Kim, SH, JOURNAL OF AIRCRAFT, v.32, no.4, pp.868 - 874, 1995-07

3336
A REFINED ANALYSIS OF VIBRATION AND DAMPING FOR ANISOTROPIC LAMINATES IN CYLINDRICAL BENDING

KOO, KN; Lee, In, JOURNAL OF SOUND AND VIBRATION, v.184, no.4, pp.553 - 566, 1995-07

3337
Navier-Stokes computation of pitch-damping coefficients using steady coning motions

Park, SH; Kwon, Jang-Hyuk, JOURNAL OF SPACECRAFT AND ROCKETS, v.41, no.5, pp.754 - 761, 2004-09

3338
Analysis of the implicit preconditioners for multigrid calculations on the high Reynolds number turbulent flows

Kim, Yoonsik; Kwon, Jang Hyuk, Computational Fluid Dynamics Journal, Vol. 12, No. 4, pp. 606-613, 2004-01

3339
Implementation of k-omega turbulence models in an implicit multigrid method

Park, SH; Kwon, Jang-Hyuk, AIAA JOURNAL, v.42, no.7, pp.1348 - 1357, 2004-07

3340
Accurate aerodynamic sensitivity analysis using adjoint equations

Sung, CH; Kwon, Jang-Hyuk, AIAA JOURNAL, v.38, no.2, pp.243 - 250, 2000-02

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