| 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
|
|
|
21 |
4 |
p. 889-905
|
artikel
|
| 2 |
An Equivalent Modeling Method for Honeycomb Sandwich Structure Based on Orthogonal Anisotropic Solid Element
|
Yuan, Jian
|
|
|
21 |
4 |
p. 957-969
|
artikel
|
| 3 |
Assessment of Cavity Covered with Porous Surface in Controlling Shock/Boundary-Layer Interactions in Hypersonic Intake
|
Jana, Tamal
|
|
|
21 |
4 |
p. 924-941
|
artikel
|
| 4 |
CFDP PDU Tunneling Service over DTN Between Heterogeneous Deep Space Communication Assets
|
Koo, Cheol Hea
|
|
|
21 |
4 |
p. 1147-1160
|
artikel
|
| 5 |
Development of Flight Control Law for Improvement of Uncommanded Lateral Motion of the Fighter Aircraft
|
Kim, Chong-Sup
|
|
|
21 |
4 |
p. 1059-1077
|
artikel
|
| 6 |
Effect of External Heat Input on Fluid Sloshing Dynamic Performance in a Liquid Oxygen Tank
|
Liu, Zhan
|
|
|
21 |
4 |
p. 879-888
|
artikel
|
| 7 |
Effect of Shape of Two-Dimensional Smooth Hump on Boundary Layer Instability
|
Park, Donghun
|
|
|
21 |
4 |
p. 906-923
|
artikel
|
| 8 |
Effects of the O/F Ratio on the Performance of a Low Thrust LOX/Methane Rocket Engine with an ElecPump-fed Cycle
|
Yu, Byungil
|
|
|
21 |
4 |
p. 1037-1046
|
artikel
|
| 9 |
Flight Control Design using Incremental Nonlinear Dynamic Inversion with Fixed-lag Smoothing Estimation
|
Ludeña Cervantes, Tito J.
|
|
|
21 |
4 |
p. 1047-1058
|
artikel
|
| 10 |
Flight Test Applications of an Improved Operational Load Monitoring Device
|
Park, Chan Yik
|
|
|
21 |
4 |
p. 970-983
|
artikel
|
| 11 |
Global Path Planning of Lunar Rover Under Static and Dynamic Constraints
|
Bai, Ji Hoon
|
|
|
21 |
4 |
p. 1105-1113
|
artikel
|
| 12 |
Guidance to Control Arrival Angle and Altitude for An Unpowered Aerial Vehicle
|
Lim, Seunghan
|
|
|
21 |
4 |
p. 1078-1091
|
artikel
|
| 13 |
Intercept Point Prediction of Ballistic Missile Defense Using Neural Network Learning
|
Lee, Jun-Yong
|
|
|
21 |
4 |
p. 1092-1104
|
artikel
|
| 14 |
Nonlinear Aeroelastic Analysis of Heated Curved Panels in Supersonic Air Flow
|
Zhou, Jian
|
|
|
21 |
4 |
p. 996-1016
|
artikel
|
| 15 |
Nonlinear Flight Mode Identification by Applying Modified Ensemble Empirical Mode Decomposition and Hilbert–Huang Transformation
|
Mokhtari, S. Abolfazl
|
|
|
21 |
4 |
p. 1161-1173
|
artikel
|
| 16 |
Nozzle Flow Influence on Forebody Aerodynamics
|
Park, Sangha
|
|
|
21 |
4 |
p. 942-956
|
artikel
|
| 17 |
Numerical Research on the Unsteady Evolution Characteristics of Blade Tip Vortex for Helicopter Rotor in Forward Flight
|
Ye, Zhou
|
|
|
21 |
4 |
p. 865-878
|
artikel
|
| 18 |
Online Safe Flight Envelope Protection for Icing Aircraft Based on Reachability Analysis
|
Yu, Zhilong
|
|
|
21 |
4 |
p. 1174-1184
|
artikel
|
| 19 |
Optimal Lunar Point Return Orbit Design and Analysis via a Numerical Three-Step Approach
|
Song, Yongjun
|
|
|
21 |
4 |
p. 1129-1146
|
artikel
|
| 20 |
Performance Evaluation on Packet Transmission for AFDX Networks Using Optimized Forward End-to-End Delay Analysis
|
Xu, Qingfei
|
|
|
21 |
4 |
p. 1114-1128
|
artikel
|
| 21 |
Performance Parameter Analysis of a Hall Effect Thruster With Modified Bohm Parameter Model
|
Cho, Min Gyoung
|
|
|
21 |
4 |
p. 1028-1036
|
artikel
|
| 22 |
The Damage Criterion Affecting Life Prediction of Fiber-Reinforced Al–Li Alloy Laminates Under Spectrum Loading
|
Meng, Weiying
|
|
|
21 |
4 |
p. 984-995
|
artikel
|
| 23 |
The Selective Zero Emission Power Systems Between NaBH4-Based Fuel Cells and Solar Cells for UAVs
|
Gang, Byeong Gyu
|
|
|
21 |
4 |
p. 1017-1027
|
artikel
|
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