| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Aerodynamic Performance Enhancement of Tiltrotor Aircraft Wings Using Double-Row Vortex Generators
|
Chen, Hao
|
|
|
22 |
4 |
p. 802-812
|
artikel
|
| 2 |
Aerodynamic Performance of the Three-Dimensional Lumped Flexibility Wing Under Wind Fluctuating Condition
|
Zhu, Mingkang
|
|
|
22 |
4 |
p. 765-778
|
artikel
|
| 3 |
A Linear Acceleration Control for Precise Trajectory Tracking Flights of a Quadrotor UAV Under High-wind Environments
|
Lee, Dasol
|
|
|
22 |
4 |
p. 898-910
|
artikel
|
| 4 |
A New Method of Reducing the Vibration Localization of the Multi-packet Whole Mistuned Bladed Disk System Using Bladed Packets
|
Kan, Xuanen
|
|
|
22 |
4 |
p. 857-865
|
artikel
|
| 5 |
A New Study on the Gap Effect of an Airfoil with Active Flap Control Based on the Overset Grid Method
|
Hu, Zhiyuan
|
|
|
22 |
4 |
p. 779-801
|
artikel
|
| 6 |
Approach Control Concepts and Optimal Vertiport Airspace Design for Urban Air Mobility (UAM) Operation
|
Song, Kyowon
|
|
|
22 |
4 |
p. 982-994
|
artikel
|
| 7 |
A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints
|
Chi, Hyo-Seon
|
|
|
22 |
4 |
p. 923-935
|
artikel
|
| 8 |
Bi-criteria Aircraft Trajectory Optimization in Implementing the Area Navigation Concept
|
Erokhin, Vyacheslav
|
|
|
22 |
4 |
p. 948-962
|
artikel
|
| 9 |
Design Optimization and Investigation of Aerodynamic Characteristics of Low Reynolds Number Airfoils
|
Arshad, Ali
|
|
|
22 |
4 |
p. 751-764
|
artikel
|
| 10 |
Development and Verification of a Fuel System to Meet Impact Resistance Performance of Rotorcraft External Auxiliary Fuel Tanks
|
Choi, Won
|
|
|
22 |
4 |
p. 974-981
|
artikel
|
| 11 |
Directional Axis Estimation including Wind Velocity for Fixed Wing UAV
|
Park, Chanhong
|
|
|
22 |
4 |
p. 995-1003
|
artikel
|
| 12 |
Dynamics and Adaptive Sliding Mode Control of a Mass-Actuated Fixed-Wing UAV
|
Qiu, Xiaoqi
|
|
|
22 |
4 |
p. 886-897
|
artikel
|
| 13 |
Estimation Technique of Minimum Energy Required for Complete Deployment of Folded Fin Under Gust Requirement (II): Considering Time Constraint
|
Jung, Suk Young
|
|
|
22 |
4 |
p. 813-823
|
artikel
|
| 14 |
Flight Simulation Training Devices: Application, Classification, and Research
|
Vidakovic, Jelena
|
|
|
22 |
4 |
p. 874-885
|
artikel
|
| 15 |
HCF Weak Link Optimization for Wide-Chord Fan Blades Based on Circumferential Stacking Line Design
|
Chen, Yong
|
|
|
22 |
4 |
p. 845-856
|
artikel
|
| 16 |
Hydrodynamic Ram Test of Composite T-Joint Structure
|
Kim, Jong Heon
|
|
|
22 |
4 |
p. 834-844
|
artikel
|
| 17 |
Improved Modeling Method for 3-Dimensional Woven Composites Using Weaving Parameters
|
Kim, Hiyeop
|
|
|
22 |
4 |
p. 824-833
|
artikel
|
| 18 |
Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer
|
Xia, Kewei
|
|
|
22 |
4 |
p. 936-947
|
artikel
|
| 19 |
Integrated Framework for Staging and Trajectory Optimization of a Launch Vehicle Considering Range Safety Operations
|
Cho, Byounggyu
|
|
|
22 |
4 |
p. 963-973
|
artikel
|
| 20 |
Inverse Design of Flow Distortion Dominated by Shock Wave Interaction with Experimental Verification
|
Yu, Kaikai
|
|
|
22 |
4 |
p. 866-873
|
artikel
|
| 21 |
Optimal Threshold of Intermittent Maneuver for Target Observability Improvement
|
Lee, Dongyeon
|
|
|
22 |
4 |
p. 911-922
|
artikel
|
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