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| 501 |
Virtual Flutter Flight Test of a Full Configuration Aircraft with Pylon/External Stores
Dong-Hyun Kim , Hyuk-Jun Kwon, In Lee , Seung-Kil Park
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.34-44, 2003 |
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| 502 |
Parallel 3-D Aerodynamic Shape Optimization on Unstructured Meshes
Sang Wook Lee , Oh Joon Kwon
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.45-52, 2003 |
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| 503 |
Nonlinear Aeroelastic Instability of a Supersonic Missile Wing with Pitch Axis Freeplay
Dong-Hyun Kim , In Lee , Seung-Kil Park
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.53-62, 2003 |
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| 504 |
Visualization and Flowfield Measurements of the Vortical Flow over a double-Delta Wing
Myong-Hwan Sohn, Young-IL Jang
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.63-74, 2003 |
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| 505 |
Ground Experiment of Spacecraft Attitude Control Using Hardware Testbed
Choongsuk Oh, Hyochoong Bang
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.75-87, 2003 |
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| 506 |
Parametric Study for the Low BVI Noise Rotor Blade Design
Changjeon Hwang, Gene Joo
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.88-98, 2003 |
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| 507 |
Three-axis Attitude Control for Flexible Spacecraft by Lyapunov Approach under Gravity Potential
Hyochoong Bang , Kwang-Hyun Lee, Hyung-Chul Lim
International Journal of Aeronautical and Space Sicences, vol. 4, no. 1, pp.99-109, 2003 |
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| 508 |
Robust and Optimal Attitude Control Law Design for Spacecraft with Inertia Uncertainties
Yonmook Park, Min-Jea Tahk
International Journal of Aeronautical and Space Sicences, vol. 3, no. 2, pp.1-12, 2002 |
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| 509 |
Sliding Mode Attitude Control for Momentum-Biased Spacecraft
Hyochoong Bang, Young Hwan Loh
International Journal of Aeronautical and Space Sicences, vol. 3, no. 2, pp.13-23, 2002 |
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| 510 |
Thermo-optic Effects of Bragg Grating Optical Temperature Sensor
Kook-Chan Ahn , Sang-Mae Lee , Gwang-Seok Lee, Seung-Bum Park
International Journal of Aeronautical and Space Sicences, vol. 3, no. 2, pp.24-30, 2002 |
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