| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Active control method for restart performances of hypersonic inlets based on energy addition
|
Liu, Hongkang
|
|
2019
|
85 |
C |
p. 481-494
|
artikel
|
| 2 |
Adaptive actuator failure compensation control for hypersonic vehicle with full state constraints
|
Xi, Yong
|
|
2019
|
85 |
C |
p. 464-473
|
artikel
|
| 3 |
Adaptive control of underactuated flight vehicles with moving mass
|
Li, Jianqing
|
|
2019
|
85 |
C |
p. 75-84
|
artikel
|
| 4 |
Aerodynamic inverse design using multifidelity models and manifold mapping
|
Du, Xiaosong
|
|
2019
|
85 |
C |
p. 371-385
|
artikel
|
| 5 |
A hollow combustor that intensifies rotating detonation
|
Wang, Yuhui
|
|
2019
|
85 |
C |
p. 113-124
|
artikel
|
| 6 |
A method to minimize stage-by-stage initial unbalance in the aero engine assembly of multistage rotors
|
Liu, Yongmeng
|
|
2019
|
85 |
C |
p. 270-276
|
artikel
|
| 7 |
A new continuous adaptive finite time guidance law against highly maneuvering targets
|
Guo, Jianguo
|
|
2019
|
85 |
C |
p. 40-47
|
artikel
|
| 8 |
Assessment of transition modeling for high Reynolds flows
|
Diakakis, Konstantinos
|
|
2019
|
85 |
C |
p. 416-428
|
artikel
|
| 9 |
A visual/inertial integrated landing guidance method for UAV landing on the ship
|
Meng, Yue
|
|
2019
|
85 |
C |
p. 474-480
|
artikel
|
| 10 |
Capturing transition with flow–structure–adaptive KDO RANS model
|
Xu, Jinglei
|
|
2019
|
85 |
C |
p. 150-157
|
artikel
|
| 11 |
Circumferentially propagating characteristic dominated by unsteady tip leakage flow in axial flow compressors
|
Li, Jichao
|
|
2019
|
85 |
C |
p. 529-543
|
artikel
|
| 12 |
Composite block backstepping trajectory tracking control for disturbed unmanned helicopters
|
Wang, Xiangyu
|
|
2019
|
85 |
C |
p. 386-398
|
artikel
|
| 13 |
Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number
|
Lu, Huawei
|
|
2019
|
85 |
C |
p. 48-60
|
artikel
|
| 14 |
Control-oriented unsteady one-dimensional model for a hydrocarbon regeneratively-cooled scramjet engine
|
Ma, Jicheng
|
|
2019
|
85 |
C |
p. 158-170
|
artikel
|
| 15 |
Coverage-based three-dimensional cooperative guidance strategy against highly maneuvering target
|
Su, Wenshan
|
|
2019
|
85 |
C |
p. 556-566
|
artikel
|
| 16 |
3D shell model for the thermo-mechanical analysis of FGM structures via imposed and calculated temperature profiles
|
Brischetto, S.
|
|
2019
|
85 |
C |
p. 125-149
|
artikel
|
| 17 |
Dynamic response of axially functionally graded beam with longitudinal–transverse coupling effect
|
Xie, Ke
|
|
2019
|
85 |
C |
p. 85-95
|
artikel
|
| 18 |
Editorial Board
|
|
|
2019
|
85 |
C |
p. ii
|
artikel
|
| 19 |
Experimental investigation of influence factors on flame holding in a supersonic combustor
|
Wang, Yanhua
|
|
2019
|
85 |
C |
p. 180-186
|
artikel
|
| 20 |
Experimental test of a 3D parameterized vane cascade with non-axisymmetric endwall
|
Guo, Zhendong
|
|
2019
|
85 |
C |
p. 429-442
|
artikel
|
| 21 |
Field-of-view constrained two-stage guidance law design for three-dimensional salvo attack of multiple missiles via an optimal control approach
|
Ai, Xiaolin
|
|
2019
|
85 |
C |
p. 334-346
|
artikel
|
| 22 |
Flow simulation and drag decomposition study of N3-X hybrid wing-body configuration
|
Kim, Hyoungjin
|
|
2019
|
85 |
C |
p. 24-39
|
artikel
|
| 23 |
Fuzzy logic based equivalent consumption optimization of a hybrid electric propulsion system for unmanned aerial vehicles
|
Xie, Ye
|
|
2019
|
85 |
C |
p. 13-23
|
artikel
|
| 24 |
Gas breakdown mitigation in satellite slip rings
|
Avino, F.
|
|
2019
|
85 |
C |
p. 229-233
|
artikel
|
| 25 |
Hydrodynamic performance in a sloshing liquid oxygen tank under different initial liquid filling levels
|
Liu, Zhan
|
|
2019
|
85 |
C |
p. 544-555
|
artikel
|
| 26 |
Ice accretion and aerodynamic effects on a multi-element airfoil under SLD icing conditions
|
Prince Raj, L.
|
|
2019
|
85 |
C |
p. 320-333
|
artikel
|
| 27 |
Integrated relative position and attitude control for spacecraft rendezvous with ISS and finite-time convergence
|
Wang, Yu
|
|
2019
|
85 |
C |
p. 234-245
|
artikel
|
| 28 |
Interaction of a plane shock wave with an area of ionization instability of discharge plasma in air
|
Lapushkina, T.A.
|
|
2019
|
85 |
C |
p. 347-358
|
artikel
|
| 29 |
Investigation on cooling effect with a combinational opposing jet and platelet transpiration concept in hypersonic flow
|
Shen, BinXian
|
|
2019
|
85 |
C |
p. 399-408
|
artikel
|
| 30 |
Investigation on wall shear stress measurement in supersonic flows with shock waves using shear-sensitive liquid crystal coating
|
Zhao, Jisong
|
|
2019
|
85 |
C |
p. 453-463
|
artikel
|
| 31 |
Kriging surrogate model applied in the mechanism study of tip leakage flow control in turbine cascade by multiple DBD plasma actuators
|
Yu, Jianyang
|
|
2019
|
85 |
C |
p. 216-228
|
artikel
|
| 32 |
Nonlinear vibration of metal foam cylindrical shells reinforced with graphene platelets
|
Wang, Yan Qing
|
|
2019
|
85 |
C |
p. 359-370
|
artikel
|
| 33 |
Optimization and control application of sensor placement in aeroservoelastic of UAV
|
Yang, Weiqi
|
|
2019
|
85 |
C |
p. 61-74
|
artikel
|
| 34 |
Preliminary aeroelastic design of composite wings subjected to critical gust loads
|
Rajpal, D.
|
|
2019
|
85 |
C |
p. 96-112
|
artikel
|
| 35 |
Pressure characteristics of a ram-RDE diffuser
|
Schwer, Douglas A.
|
|
2019
|
85 |
C |
p. 187-198
|
artikel
|
| 36 |
Recurrence network analysis for uncovering dynamic transition of thermo-acoustic instability of supercritical hydrocarbon fuel flow
|
Zan, Hao
|
|
2019
|
85 |
C |
p. 1-12
|
artikel
|
| 37 |
Research on gravity vertical deflection on attitude of position and orientation system and compensation method
|
Zhu, Zhuangsheng
|
|
2019
|
85 |
C |
p. 495-504
|
artikel
|
| 38 |
Robust optimization of impulsive orbit transfers under actuation uncertainties
|
Sadegh Mohammadi, Mohammad
|
|
2019
|
85 |
C |
p. 246-258
|
artikel
|
| 39 |
Robust trajectory tracking controller for quadrotor helicopter based on a novel composite control scheme
|
Zhang, Juqian
|
|
2019
|
85 |
C |
p. 199-215
|
artikel
|
| 40 |
Roughness effect on shock wave boundary layer interaction area in compressor fan blades passage
|
Szwaba, Ryszard
|
|
2019
|
85 |
C |
p. 171-179
|
artikel
|
| 41 |
Sandbraking. A technique for landing large payloads on Mars using the sands of Phobos
|
Arias, Francisco J.
|
|
2019
|
85 |
C |
p. 409-415
|
artikel
|
| 42 |
Scaled sequential threshold least-squares (S2TLS) algorithm for sparse regression modeling and flight load prediction
|
Zhu, Shengwei
|
|
2019
|
85 |
C |
p. 514-528
|
artikel
|
| 43 |
Simulation of helicopter ditching using smoothed particle hydrodynamics
|
Woodgate, Mark A.
|
|
2019
|
85 |
C |
p. 277-292
|
artikel
|
| 44 |
Stability enhancement using a new hybrid casing treatment in an axial flow compressor
|
Li, Jichao
|
|
2019
|
85 |
C |
p. 305-319
|
artikel
|
| 45 |
Three-dimensional nonlinear gravity assisted aiming point guidance
|
H. Ramesh, Shashank
|
|
2019
|
85 |
C |
p. 505-513
|
artikel
|
| 46 |
Trim investigation for coaxial rigid rotor helicopters using an improved aerodynamic interference model
|
Yuan, Ye
|
|
2019
|
85 |
C |
p. 293-304
|
artikel
|
| 47 |
Unscented Kalman filters for range-only cooperative localization of swarms of munitions in three-dimensional flight
|
Burchett, Bradley T.
|
|
2019
|
85 |
C |
p. 259-269
|
artikel
|
| 48 |
Vortex dynamic mechanism of curved blade affecting flow loss in compressor cascade during corner stall process
|
Kan, Xiaoxu
|
|
2019
|
85 |
C |
p. 443-452
|
artikel
|
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