| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Air-breathing pulsed detonation thrust module: Numerical simulations and firing tests
|
Frolov, S.M.
|
|
2019
|
89 |
C |
p. 275-287
|
artikel
|
| 2 |
An in-depth numerical investigation of a supersonic cavity-ramp flow with DDES method
|
Wu, Zhengyuan
|
|
2019
|
89 |
C |
p. 253-263
|
artikel
|
| 3 |
An on-line guidance algorithm for high L/D hypersonic reentry vehicles
|
Zang, Luyao
|
|
2019
|
89 |
C |
p. 150-162
|
artikel
|
| 4 |
Anti-tangle control of tethered space robots using linear motion of tether offset
|
Wang, Bingheng
|
|
2019
|
89 |
C |
p. 163-174
|
artikel
|
| 5 |
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
|
Peng, Jun
|
|
2019
|
89 |
C |
p. 299-306
|
artikel
|
| 6 |
C-loss based extreme learning machine for estimating power of small-scale turbojet engine
|
Zhao, Yong-Ping
|
|
2019
|
89 |
C |
p. 407-419
|
artikel
|
| 7 |
Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket
|
Di Martino, G.D.
|
|
2019
|
89 |
C |
p. 431-444
|
artikel
|
| 8 |
De-icing of fuel/oil heat exchange systems via fuel flow direction switching device
|
Moon, Chanhee
|
|
2019
|
89 |
C |
p. 77-88
|
artikel
|
| 9 |
Design concept for In-Drag Sail with individually controllable elements
|
Qu, Qingyu
|
|
2019
|
89 |
C |
p. 382-391
|
artikel
|
| 10 |
Distributed onboard mission planning for multi-satellite systems
|
Zheng, Zixuan
|
|
2019
|
89 |
C |
p. 111-122
|
artikel
|
| 11 |
Disturbance observer-based gain adaptation high-order sliding mode control of hypersonic vehicles
|
Yin, Xiaomeng
|
|
2019
|
89 |
C |
p. 19-30
|
artikel
|
| 12 |
Dynamics modeling and trajectory optimization for unmanned aerial-aquatic vehicle diving into the water
|
Wu, Yu
|
|
2019
|
89 |
C |
p. 220-229
|
artikel
|
| 13 |
Editorial Board
|
|
|
2019
|
89 |
C |
p. ii
|
artikel
|
| 14 |
Fixed-time trajectory tracking for a quadrotor with external disturbances: A flatness-based sliding mode control approach
|
Ai, Xiaolin
|
|
2019
|
89 |
C |
p. 58-76
|
artikel
|
| 15 |
High-order ESO based output feedback dynamic surface control for quadrotors under position constraints and uncertainties
|
Shao, Xingling
|
|
2019
|
89 |
C |
p. 288-298
|
artikel
|
| 16 |
Implicit large eddy simulation of vitiation effects in supersonic air/H2 combustion
|
Karaca, Mehmet
|
|
2019
|
89 |
C |
p. 89-99
|
artikel
|
| 17 |
Installation aerodynamics of civil aero-engine exhaust systems
|
Otter, John J.
|
|
2019
|
89 |
C |
p. 345-355
|
artikel
|
| 18 |
Integrated guidance and control design for the hypersonic interceptor based on adaptive incremental backstepping technique
|
Chang, Jing
|
|
2019
|
89 |
C |
p. 318-332
|
artikel
|
| 19 |
Integrated methodology for the prediction of helicopter rotor noise at mission level
|
Vouros, Stavros
|
|
2019
|
89 |
C |
p. 136-149
|
artikel
|
| 20 |
Investigations on the accurate prediction of supersonic shear layers for detached eddy simulation
|
Guo, Peixu
|
|
2019
|
89 |
C |
p. 46-57
|
artikel
|
| 21 |
Kalman-filter based online system identification of fixed-wing aircraft in upset condition
|
Seo, Gwang-gyo
|
|
2019
|
89 |
C |
p. 307-317
|
artikel
|
| 22 |
Large eddy simulation of transverse single/double jet in supersonic crossflow
|
Zhao, Majie
|
|
2019
|
89 |
C |
p. 31-45
|
artikel
|
| 23 |
Large eddy simulation of turbulent jet controlled by two pulsed jets: Effect of forcing frequency
|
Kong, Bo
|
|
2019
|
89 |
C |
p. 356-369
|
artikel
|
| 24 |
Mapped Chebyshev pseudospectral methods for optimal trajectory planning of differentially flat hypersonic vehicle systems
|
Wang, Jianying
|
|
2019
|
89 |
C |
p. 420-430
|
artikel
|
| 25 |
Modified under-actuated quadrotor model for forwarding flight in the presence of ground effect
|
Keshavarzian, Hasan
|
|
2019
|
89 |
C |
p. 242-252
|
artikel
|
| 26 |
Multiple missiles cooperative guidance with simultaneous attack requirement under directed topologies
|
Lyu, Teng
|
|
2019
|
89 |
C |
p. 100-110
|
artikel
|
| 27 |
Numerical investigation on the biomimetic trailing edge of a high-subsonic turbine blade
|
Luo, Yuxi
|
|
2019
|
89 |
C |
p. 230-241
|
artikel
|
| 28 |
Open and closed loop gust loads analyses for a flying wing configuration with variable longitudinal stability
|
Voß, A.
|
|
2019
|
89 |
C |
p. 1-10
|
artikel
|
| 29 |
Performance assessment of an integrated power generation and refrigeration system on hypersonic vehicles
|
Cheng, Kunlin
|
|
2019
|
89 |
C |
p. 192-203
|
artikel
|
| 30 |
Performance comparison of oxidizer injectors in a 1-kN paraffin-fueled hybrid rocket motor
|
Bouziane, M.
|
|
2019
|
89 |
C |
p. 392-406
|
artikel
|
| 31 |
Robust aircraft trajectory planning under uncertain convective environments with optimal control and rapidly developing thunderstorms
|
González-Arribas, Daniel
|
|
2019
|
89 |
C |
p. 445-459
|
artikel
|
| 32 |
Shock response prediction of the typical structure in spacecraft based on the hybrid modeling techniques
|
Zhao, Hongda
|
|
2019
|
89 |
C |
p. 460-467
|
artikel
|
| 33 |
Structural design and verification of an innovative whole adaptive variable camber wing
|
Zhao, Anmin
|
|
2019
|
89 |
C |
p. 11-18
|
artikel
|
| 34 |
Swing angle estimation for multicopter slung load applications
|
de Angelis, Emanuele L.
|
|
2019
|
89 |
C |
p. 264-274
|
artikel
|
| 35 |
Time-coordination entry guidance for multi-hypersonic vehicles
|
Li, Zhenhua
|
|
2019
|
89 |
C |
p. 123-135
|
artikel
|
| 36 |
Transonic buffet control by rearward Buffet Breather on supercritical airfoil and wing
|
Jiang, Runpei
|
|
2019
|
89 |
C |
p. 204-219
|
artikel
|
| 37 |
Two-stage filter for inertia characteristics estimation of high-speed tumbling targets
|
Ma, Chuan
|
|
2019
|
89 |
C |
p. 333-344
|
artikel
|
| 38 |
Unsteady actuation of counter-flowing wall jets for gust load attenuation
|
Al-Battal, Nader H.
|
|
2019
|
89 |
C |
p. 175-191
|
artikel
|
| 39 |
Validation of an integrated simulation model for aircraft noise and engine emissions
|
Filippone, Antonio
|
|
2019
|
89 |
C |
p. 370-381
|
artikel
|
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