| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Ablation Experiments of Ultra-High-Temperature Ceramic Coating on Carbon–Carbon Composite Using ICP Plasma Wind Tunnel
|
Chinnaraj, Rajesh Kumar
|
|
|
|
4 |
p. 889-905
|
artikel
|
| 2 |
A Development and Assessment of Variable-Incidence Angle Vortex Generator at Low Reynolds Number of ~ 5×104
|
Kim, Ho-Hyun
|
|
2018
|
|
4 |
p. 836-842
|
artikel
|
| 3 |
Aerodynamic Analysis of High-Speed Compound Unmanned Rotorcraft Using an Unstructured Flow Solver
|
Park, Sang Hyun
|
|
|
|
4 |
p. 1077-1085
|
artikel
|
| 4 |
Aerodynamic Performance Enhancement of Tiltrotor Aircraft Wings Using Double-Row Vortex Generators
|
Chen, Hao
|
|
|
|
4 |
p. 802-812
|
artikel
|
| 5 |
Aerodynamic Performance of the Three-Dimensional Lumped Flexibility Wing Under Wind Fluctuating Condition
|
Zhu, Mingkang
|
|
|
|
4 |
p. 765-778
|
artikel
|
| 6 |
Aerodynamics and Propulsive Efficiency of a Blended-Wing-Body Aircraft with Distributed Propulsion System During Takeoff
|
Lian, Zengyan
|
|
2018
|
|
4 |
p. 799-804
|
artikel
|
| 7 |
Aeroservoelastic Characteristics of a Corrugated Morphing Control Surface
|
Soneda, Kensuke
|
|
|
|
4 |
p. 723-733
|
artikel
|
| 8 |
A Hybrid Dynamic Window Approach for Collision Avoidance of VTOL UAVs
|
Moon, Jungho
|
|
2018
|
|
4 |
p. 889-903
|
artikel
|
| 9 |
A Linear Acceleration Control for Precise Trajectory Tracking Flights of a Quadrotor UAV Under High-wind Environments
|
Lee, Dasol
|
|
|
|
4 |
p. 898-910
|
artikel
|
| 10 |
Analysis of Characteristics of Swirling Spray of the Ammonium Dinitramide (ADN)-Based Green Monopropellant
|
Chen, Jun
|
|
2018
|
|
4 |
p. 926-931
|
artikel
|
| 11 |
Analysis of Flow Oscillation Due to Sidewall of Three-Dimensional Supersonic Open Cavity Flow
|
Kim, T. U.
|
|
2019
|
|
4 |
p. 839-849
|
artikel
|
| 12 |
An Efficient Power-On Base Pressure Prediction Inside the Tube Using Axisymmetric and Quasi-Steady Computation
|
Lee, Jae Eun
|
|
2019
|
|
4 |
p. 831-838
|
artikel
|
| 13 |
An Equivalent Modeling Method for Honeycomb Sandwich Structure Based on Orthogonal Anisotropic Solid Element
|
Yuan, Jian
|
|
|
|
4 |
p. 957-969
|
artikel
|
| 14 |
A New Method of Reducing the Vibration Localization of the Multi-packet Whole Mistuned Bladed Disk System Using Bladed Packets
|
Kan, Xuanen
|
|
|
|
4 |
p. 857-865
|
artikel
|
| 15 |
A New Study on the Gap Effect of an Airfoil with Active Flap Control Based on the Overset Grid Method
|
Hu, Zhiyuan
|
|
|
|
4 |
p. 779-801
|
artikel
|
| 16 |
An Immersed Boundary Method for Conjugate Heat Transfer Involving Melting/Solidification
|
Ahn, Joon
|
|
|
|
4 |
p. 1032-1041
|
artikel
|
| 17 |
An Implicit Multicloud Convergence Accelerator for Compressible Flows
|
Rhee, Jaesang
|
|
|
|
4 |
p. 1136-1146
|
artikel
|
| 18 |
A Numerical Study on the Effect of the Umbilical Plate on Longitudinal Controllability of a Low Aspect Ratio Launch Vehicle
|
Kim, Younghoon
|
|
2019
|
|
4 |
p. 870-878
|
artikel
|
| 19 |
Approach Control Concepts and Optimal Vertiport Airspace Design for Urban Air Mobility (UAM) Operation
|
Song, Kyowon
|
|
|
|
4 |
p. 982-994
|
artikel
|
| 20 |
A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints
|
Chi, Hyo-Seon
|
|
|
|
4 |
p. 923-935
|
artikel
|
| 21 |
A Precision Landing Test on Motion Platform and Shipboard of a Tilt-Rotor UAV Based on RTK-GNSS
|
Kang, Youngshin
|
|
2018
|
|
4 |
p. 994-1005
|
artikel
|
| 22 |
Ascent Guidance Trajectory Optimization Using Evolutionary Algorithm Considering Engine Gimbal and Aerodynamic Control
|
Murakami, Masaaki
|
|
|
|
4 |
p. 775-783
|
artikel
|
| 23 |
Assessment of Cavity Covered with Porous Surface in Controlling Shock/Boundary-Layer Interactions in Hypersonic Intake
|
Jana, Tamal
|
|
|
|
4 |
p. 924-941
|
artikel
|
| 24 |
A Study on Aero-Engine Direct Thrust Control with Nonlinear Model Predictive Control Based on Deep Neural Network
|
Zheng, Qiangang
|
|
2019
|
|
4 |
p. 933-939
|
artikel
|
| 25 |
A Through-Flow Analysis for Application to Off-Design of Axial Gas Turbines
|
Song, Jeonghwan
|
|
|
|
4 |
p. 1086-1101
|
artikel
|
| 26 |
Attitude Control of Momentum-Biased Satellites Equipped with Control Moment Gyroscopes
|
Jin, Jaehyun
|
|
2019
|
|
4 |
p. 987-996
|
artikel
|
| 27 |
Bi-criteria Aircraft Trajectory Optimization in Implementing the Area Navigation Concept
|
Erokhin, Vyacheslav
|
|
|
|
4 |
p. 948-962
|
artikel
|
| 28 |
Biologically Inspired Dynamic Soaring Maneuvers for an Unmanned Air Vehicle Capable of Sweep Morphing
|
Mir, Imran
|
|
2018
|
|
4 |
p. 1006-1016
|
artikel
|
| 29 |
Broadband Laser Ultrasonic Excitation and Multi-band Sensing for Hierarchical Automatic Damage Visualization
|
Thai, Mai-Thanh
|
|
2019
|
|
4 |
p. 913-932
|
artikel
|
| 30 |
CFDP PDU Tunneling Service over DTN Between Heterogeneous Deep Space Communication Assets
|
Koo, Cheol Hea
|
|
|
|
4 |
p. 1147-1160
|
artikel
|
| 31 |
Closed-Loop Bifurcation Analysis for a Novel Moving Mass Flight Vehicle
|
Liu, Zhitao
|
|
2018
|
|
4 |
p. 962-975
|
artikel
|
| 32 |
Coarray Fortran Parallel Implementation of a Finite Volume Method-Based Aircraft Ice Accretion Simulation Code
|
Raj, L. Prince
|
|
|
|
4 |
p. 1124-1135
|
artikel
|
| 33 |
Computational Study on the Steady Loading Noise of Drone Propellers: Noise Source Modeling with the Lattice Boltzmann Method
|
Park, Chun Hyuk
|
|
2019
|
|
4 |
p. 858-869
|
artikel
|
| 34 |
Convolutional Neural Network-Based Multi-Target Detection and Recognition Method for Unmanned Airborne Surveillance Systems
|
Kim, Sang-Hyeon
|
|
2019
|
|
4 |
p. 1038-1046
|
artikel
|
| 35 |
Cooperative sUAV Collision Avoidance Based on Satisficing Theory
|
Kim, Namwoo
|
|
2019
|
|
4 |
p. 978-986
|
artikel
|
| 36 |
Correction Technique of Inertial Force and Moment in Direct Force Measuring Test of Dynamic Aerodynamic Performance of Airfoils
|
Jiao, Yuqin
|
|
|
|
4 |
p. 692-701
|
artikel
|
| 37 |
Correction to: Simulation of Counter-Rotating Vortex Pairs on a Triangular-Flapped Wing with Flap-Tip Free Vortex Modeling
|
Kang, Woo-Ram
|
|
2018
|
|
4 |
p. 816
|
artikel
|
| 38 |
Correlation Between Mechanical Properties Degradation and Discoloration of Epoxy Polymer by Solar Radiation Exposure
|
Lee, Sangbong
|
|
2018
|
|
4 |
p. 843-854
|
artikel
|
| 39 |
Deflection Analysis of Flexible Cantilever Beam with a Drop Impact
|
Kim, Chanho
|
|
|
|
4 |
p. 1054-1062
|
artikel
|
| 40 |
Delayed Detached-Eddy Simulation of Subsonic Axisymmetric Base Flow
|
Jeong, Minjae
|
|
|
|
4 |
p. 1160-1170
|
artikel
|
| 41 |
Design and Analysis of Micro-Vibration Isolation System for Digital Image Correlation System-Based Structural Health Monitoring
|
Doan, Nguyen Vu
|
|
|
|
4 |
p. 711-722
|
artikel
|
| 42 |
Design Optimization and Investigation of Aerodynamic Characteristics of Low Reynolds Number Airfoils
|
Arshad, Ali
|
|
|
|
4 |
p. 751-764
|
artikel
|
| 43 |
Development and Flight Test of Affordable Scientific Balloon System Suitable for Sea Recovery
|
Kang, Jungpyo
|
|
2019
|
|
4 |
p. 1024-1037
|
artikel
|
| 44 |
Development and Verification of a Fuel System to Meet Impact Resistance Performance of Rotorcraft External Auxiliary Fuel Tanks
|
Choi, Won
|
|
|
|
4 |
p. 974-981
|
artikel
|
| 45 |
Development of Flight Control Law for Improvement of Uncommanded Lateral Motion of the Fighter Aircraft
|
Kim, Chong-Sup
|
|
|
|
4 |
p. 1059-1077
|
artikel
|
| 46 |
Development of the Snapshot Method for Six Degree-of-Freedom Flight Dynamics Simulation of a High Aspect Ratio Wing Aircraft
|
Been, Youngbeen
|
|
2018
|
|
4 |
p. 904-919
|
artikel
|
| 47 |
Directional Axis Estimation including Wind Velocity for Fixed Wing UAV
|
Park, Chanhong
|
|
|
|
4 |
p. 995-1003
|
artikel
|
| 48 |
Direct-Numerical Simulation with the Stability Theory for Turbulent Transition in Hypersonic Boundary Layer
|
Bae, Hajun
|
|
|
|
4 |
p. 1004-1014
|
artikel
|
| 49 |
Dynamic Characteristics of a Coaxial Jet–Swirl Injector with External Excitation
|
Bae, Jinhyun
|
|
2018
|
|
4 |
p. 920-925
|
artikel
|
| 50 |
Dynamics and Adaptive Sliding Mode Control of a Mass-Actuated Fixed-Wing UAV
|
Qiu, Xiaoqi
|
|
|
|
4 |
p. 886-897
|
artikel
|
| 51 |
Effect of External Heat Input on Fluid Sloshing Dynamic Performance in a Liquid Oxygen Tank
|
Liu, Zhan
|
|
|
|
4 |
p. 879-888
|
artikel
|
| 52 |
Effect of Inlet Boundary Layer Suction on Flow Distortion in Subsonic Diffusing S-Duct
|
Lee, Jihyeong
|
|
2019
|
|
4 |
p. 850-857
|
artikel
|
| 53 |
Effect of Non-isothermal Phase Change on Multiple Bubble Pulsations
|
Kim, Seonghak
|
|
|
|
4 |
p. 1063-1076
|
artikel
|
| 54 |
Effect of Shape of Two-Dimensional Smooth Hump on Boundary Layer Instability
|
Park, Donghun
|
|
|
|
4 |
p. 906-923
|
artikel
|
| 55 |
Effects of RANS Turbulence Models on Aerodynamics of Slender-Bodied Launch Vehicles with Protuberance
|
Tsutsui, Fumiya
|
|
|
|
4 |
p. 670-679
|
artikel
|
| 56 |
Effects of the O/F Ratio on the Performance of a Low Thrust LOX/Methane Rocket Engine with an ElecPump-fed Cycle
|
Yu, Byungil
|
|
|
|
4 |
p. 1037-1046
|
artikel
|
| 57 |
Effects of Thermo-chemical Models on Linear Stability Analysis of Chemically Reacting Hypersonic Boundary Layers
|
Park, Jaeyoung
|
|
|
|
4 |
p. 985-1003
|
artikel
|
| 58 |
Estimation Method for Pitching Moment Non-linearities of Cranked Arrow Wing at Low Speed
|
Ishibashi, Hiroki
|
|
|
|
4 |
p. 680-691
|
artikel
|
| 59 |
Estimation Technique of Minimum Energy Required for Complete Deployment of Folded Fin Under Gust Requirement (II): Considering Time Constraint
|
Jung, Suk Young
|
|
|
|
4 |
p. 813-823
|
artikel
|
| 60 |
Flight Control Design using Incremental Nonlinear Dynamic Inversion with Fixed-lag Smoothing Estimation
|
Ludeña Cervantes, Tito J.
|
|
|
|
4 |
p. 1047-1058
|
artikel
|
| 61 |
Flight Performance Optimization Considering Environmental Impact Under Multi-RTA Constraints
|
Gu, Runping
|
|
2019
|
|
4 |
p. 964-977
|
artikel
|
| 62 |
Flight Simulation Training Devices: Application, Classification, and Research
|
Vidakovic, Jelena
|
|
|
|
4 |
p. 874-885
|
artikel
|
| 63 |
Flight Test Applications of an Improved Operational Load Monitoring Device
|
Park, Chan Yik
|
|
|
|
4 |
p. 970-983
|
artikel
|
| 64 |
Formation Control of Multiple UAVs Incorporating Extended State Observer-Based Model Predictive Approach
|
Zhang, Boyang
|
|
2019
|
|
4 |
p. 953-963
|
artikel
|
| 65 |
Free Vibration Analysis of Graphene Platelets–Reinforced Composites Plates in Thermal Environment Based on Higher-Order Shear Deformation Plate Theory
|
Qaderi, Saeedeh
|
|
2019
|
|
4 |
p. 902-912
|
artikel
|
| 66 |
Fuel Quantity Estimation of Aircraft Supplementary Tank Using Markov Chain Monte Carlo Method
|
Lee, Jaewook
|
|
2019
|
|
4 |
p. 1047-1054
|
artikel
|
| 67 |
Global Path Planning of Lunar Rover Under Static and Dynamic Constraints
|
Bai, Ji Hoon
|
|
|
|
4 |
p. 1105-1113
|
artikel
|
| 68 |
Guidance to Control Arrival Angle and Altitude for An Unpowered Aerial Vehicle
|
Lim, Seunghan
|
|
|
|
4 |
p. 1078-1091
|
artikel
|
| 69 |
HCF Weak Link Optimization for Wide-Chord Fan Blades Based on Circumferential Stacking Line Design
|
Chen, Yong
|
|
|
|
4 |
p. 845-856
|
artikel
|
| 70 |
Hydrodynamic Ram Test of Composite T-Joint Structure
|
Kim, Jong Heon
|
|
|
|
4 |
p. 834-844
|
artikel
|
| 71 |
Improved Modeling Method for 3-Dimensional Woven Composites Using Weaving Parameters
|
Kim, Hiyeop
|
|
|
|
4 |
p. 824-833
|
artikel
|
| 72 |
Improvement of DOD/DOA Estimation for Bistatic MIMO Radar
|
Paik, Ji Woong
|
|
2019
|
|
4 |
p. 997-1009
|
artikel
|
| 73 |
Initial Error Dispersion and Midcourse Correction Maneuver Analysis of the Lunar Orbiter
|
Bae, Jonghee
|
|
2018
|
|
4 |
p. 1041-1051
|
artikel
|
| 74 |
Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer
|
Xia, Kewei
|
|
|
|
4 |
p. 936-947
|
artikel
|
| 75 |
Integrated Framework for Staging and Trajectory Optimization of a Launch Vehicle Considering Range Safety Operations
|
Cho, Byounggyu
|
|
|
|
4 |
p. 963-973
|
artikel
|
| 76 |
Integrated Optimal Guidance for Reentry and Landing of a Rocket Using Multi-Phase Pseudo-Spectral Convex Optimization
|
Hwang, Junsub
|
|
|
|
4 |
p. 766-774
|
artikel
|
| 77 |
Integrated Risk Management Method Development for Multiple Aerospace Projects Using a Single Index Expression
|
Ahn, Hyojung
|
|
2018
|
|
4 |
p. 1052-1062
|
artikel
|
| 78 |
Intercept Point Prediction of Ballistic Missile Defense Using Neural Network Learning
|
Lee, Jun-Yong
|
|
|
|
4 |
p. 1092-1104
|
artikel
|
| 79 |
Inverse Design of Flow Distortion Dominated by Shock Wave Interaction with Experimental Verification
|
Yu, Kaikai
|
|
|
|
4 |
p. 866-873
|
artikel
|
| 80 |
Investigation of Hydrodynamic Ram Behavior Using Newly Established HRam Gun System
|
Seo, Bohwi
|
|
2018
|
|
4 |
p. 855-862
|
artikel
|
| 81 |
Investigation on Excitation Equivalence Technique for Thin-Walled Panel Based on Pseudo-excitation Method
|
Zhou, Hong-wei
|
|
|
|
4 |
p. 702-710
|
artikel
|
| 82 |
Layout Optimization for Blended Wing Body Aircraft Structure
|
Zhu, Wensheng
|
|
2019
|
|
4 |
p. 879-890
|
artikel
|
| 83 |
Linear Pseudospectral Entry Guidance Algorithm Using Differential Flat Output for High Lift-to-Drag Ratio Entry Vehicle
|
Wang, Chongchong
|
|
|
|
4 |
p. 755-765
|
artikel
|
| 84 |
Longitudinal System Identification of an Avian-Type UAV Considering Characteristics of Actuator
|
Gim, Hakseong
|
|
2018
|
|
4 |
p. 1017-1026
|
artikel
|
| 85 |
Maneuvering Target Tracking Using LOS and Fuzzy Input Estimator
|
Chen, Yi-Wei
|
|
2018
|
|
4 |
p. 878-888
|
artikel
|
| 86 |
Measurements of the Laminar-Separated Region on the Airfoil with Actively Deflected Flap
|
Akama, Yuta
|
|
|
|
4 |
p. 660-669
|
artikel
|
| 87 |
Modeling of Profile Error and Application to a Low Reynolds Number Airfoil
|
Lee, Jaehun
|
|
2018
|
|
4 |
p. 817-827
|
artikel
|
| 88 |
Nonlinear Aeroelastic Analysis of Heated Curved Panels in Supersonic Air Flow
|
Zhou, Jian
|
|
|
|
4 |
p. 996-1016
|
artikel
|
| 89 |
Nonlinear Flight Mode Identification by Applying Modified Ensemble Empirical Mode Decomposition and Hilbert–Huang Transformation
|
Mokhtari, S. Abolfazl
|
|
|
|
4 |
p. 1161-1173
|
artikel
|
| 90 |
Nonlinear Model Predictive Control for Near-Space Interceptor Based on Finite Time Disturbance Observer
|
Guo, Chao
|
|
2018
|
|
4 |
p. 945-961
|
artikel
|
| 91 |
Nozzle Flow Influence on Forebody Aerodynamics
|
Park, Sangha
|
|
|
|
4 |
p. 942-956
|
artikel
|
| 92 |
Numerical and Experimental Analysis of Three-Dimensional Boundary-Layer Transition Induced by Isolated Cylindrical Roughness Elements
|
Ishida, Takahiro
|
|
|
|
4 |
p. 649-659
|
artikel
|
| 93 |
Numerical Research on the Unsteady Evolution Characteristics of Blade Tip Vortex for Helicopter Rotor in Forward Flight
|
Ye, Zhou
|
|
|
|
4 |
p. 865-878
|
artikel
|
| 94 |
Numerical Simulations of Blast Wave Propagation After a High-Energy Explosion
|
Yu, Wanli
|
|
|
|
4 |
p. 1042-1053
|
artikel
|
| 95 |
Numerical Study of the Effects of a Counterflow Jet on the Drag Reduction of a Blunt Body in a Hypersonic Flow
|
Yoon, Hee
|
|
2018
|
|
4 |
p. 828-835
|
artikel
|
| 96 |
Numerical Study of Wing Tip-Mounted Tractor and Pusher Propellers in Comparison with Conventional Layout
|
Chandukrishna, Y.
|
|
|
|
4 |
p. 1111-1123
|
artikel
|
| 97 |
Online Safe Flight Envelope Protection for Icing Aircraft Based on Reachability Analysis
|
Yu, Zhilong
|
|
|
|
4 |
p. 1174-1184
|
artikel
|
| 98 |
Optimal Lunar Point Return Orbit Design and Analysis via a Numerical Three-Step Approach
|
Song, Yongjun
|
|
|
|
4 |
p. 1129-1146
|
artikel
|
| 99 |
Optimal Policy of Pitch-Hold Phase for Mine Detection of UAV Based on Mixed-Integer Linear Programming
|
Lee, Sangmin
|
|
|
|
4 |
p. 746-754
|
artikel
|
| 100 |
Optimal Threshold of Intermittent Maneuver for Target Observability Improvement
|
Lee, Dongyeon
|
|
|
|
4 |
p. 911-922
|
artikel
|
| 101 |
Optimized Ristorcelli’s Compressibility Correction to the k-ω SST Turbulence Model for Base Flow Analysis
|
Kim, Donguk
|
|
|
|
4 |
p. 1147-1159
|
artikel
|
| 102 |
Performance Analysis of Flash LiDAR Based TRN Using Different Correlation Functions
|
Yoon, Indo
|
|
2018
|
|
4 |
p. 986-993
|
artikel
|
| 103 |
Performance Analysis of Passive Magnetic Pointing Method for Implementation of Directional Antennas on CubeSats
|
Kang, Jin S.
|
|
|
|
4 |
p. 734-745
|
artikel
|
| 104 |
Performance Evaluation on Packet Transmission for AFDX Networks Using Optimized Forward End-to-End Delay Analysis
|
Xu, Qingfei
|
|
|
|
4 |
p. 1114-1128
|
artikel
|
| 105 |
Performance Parameter Analysis of a Hall Effect Thruster With Modified Bohm Parameter Model
|
Cho, Min Gyoung
|
|
|
|
4 |
p. 1028-1036
|
artikel
|
| 106 |
Review of More Electric Engines for Civil Aircraft
|
Liu, Yixiong
|
|
|
|
4 |
p. 784-793
|
artikel
|
| 107 |
Robust Stabilization Technique for the Leader Steering Slung-Load System/Using Sliding Mode Control
|
Oh, Hyun-Shik
|
|
2018
|
|
4 |
p. 932-944
|
artikel
|
| 108 |
Selected Papers from the 13th Asian Computational Fluid Dynamics Conference (ACFD 2022) (Jeju, Republic of Korea, Oct. 16th–19th, 2022)
|
Kim, Chongam
|
|
|
|
4 |
p. 971
|
artikel
|
| 109 |
Selected Papers from the 12th Asia–Pacific International Symposium on Aerospace Technology (APISAT 2021) (Jeju, Republic of Korea, Nov. 15th–17th, 2021)
|
Goo, Nam Seo
|
|
|
|
4 |
p. 647-648
|
artikel
|
| 110 |
Self-Tuning Proportional Double Derivative-Like Neural Network Controller for a Quadrotor
|
Tran, Thi-Trang
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