| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A composite impact-time-control guidance law and simultaneous arrival
|
Cheng, Zhongtao
|
|
2018
|
80 |
C |
p. 403-412
|
artikel
|
| 2 |
A comprehensive high-order solver verification methodology for free fluid flows
|
Navah, Farshad
|
|
2018
|
80 |
C |
p. 101-126
|
artikel
|
| 3 |
Adaptive RBF observer-sliding mode controller design for a two dimensional aeroelastic system with unsteady aerodynamics
|
Yuan, Jiaxin
|
|
2018
|
80 |
C |
p. 482-495
|
artikel
|
| 4 |
Aeroelastic analysis of functionally graded rotating blades reinforced with graphene nanoplatelets in supersonic flow
|
Bahaadini, Reza
|
|
2018
|
80 |
C |
p. 381-391
|
artikel
|
| 5 |
A new Gaussian mixture method with exactly exploiting the negative information for GMTI radar tracking in a low-observable environment
|
Gong, Liyun
|
|
2018
|
80 |
C |
p. 1-10
|
artikel
|
| 6 |
Autonomous entry guidance using Linear Pseudospectral Model Predictive Control
|
Yang, Liang
|
|
2018
|
80 |
C |
p. 38-55
|
artikel
|
| 7 |
Autonomous orbit and attitude determination for Earth satellites using images of regular-shaped ground objects
|
Li, Muzi
|
|
2018
|
80 |
C |
p. 192-202
|
artikel
|
| 8 |
Combustion characteristics of hydrogen and cracked kerosene in a DLR scramjet combustor using hybrid RANS/LES method
|
Shin, Junsu
|
|
2018
|
80 |
C |
p. 433-444
|
artikel
|
| 9 |
Comparison of studies on flow and flame structures in different swirl combustors
|
Zhou, L.X.
|
|
2018
|
80 |
C |
p. 29-37
|
artikel
|
| 10 |
Conceptual design and CFD analysis of a new prototype of agricultural aircraft
|
Bravo-Mosquera, Pedro David
|
|
2018
|
80 |
C |
p. 156-176
|
artikel
|
| 11 |
Cooperative interception strategy for multiple inferior missiles against one highly maneuvering target
|
Su, Wenshan
|
|
2018
|
80 |
C |
p. 91-100
|
artikel
|
| 12 |
Criteria for designing low-loss and wide operation range variable inlet guide vanes
|
Shi, Hengtao
|
|
2018
|
80 |
C |
p. 177-191
|
artikel
|
| 13 |
Deep learning based trajectory optimization for UAV aerial refueling docking under bow wave
|
Liu, Yiheng
|
|
2018
|
80 |
C |
p. 392-402
|
artikel
|
| 14 |
Design of mistuning patterns to control the vibration amplitude of unstable rotor blades
|
Corral, Roque
|
|
2018
|
80 |
C |
p. 20-28
|
artikel
|
| 15 |
Dynamic surface control design of post-stall maneuver under unsteady aerodynamics
|
Lyu, Yongxi
|
|
2018
|
80 |
C |
p. 269-280
|
artikel
|
| 16 |
Editorial Board
|
|
|
2018
|
80 |
C |
p. ii
|
artikel
|
| 17 |
Effect of cavity geometry on fuel transport and mixing processes in a scramjet combustor
|
Cai, Zun
|
|
2018
|
80 |
C |
p. 309-314
|
artikel
|
| 18 |
Effect of design parameters on the mass of a variable-span morphing wing based on finite element structural analysis and optimization
|
Santos, Pedro D.R.
|
|
2018
|
80 |
C |
p. 587-603
|
artikel
|
| 19 |
Efficient numerical algorithm of profust reliability analysis: An application to wing box structure
|
Feng, Kaixuan
|
|
2018
|
80 |
C |
p. 203-211
|
artikel
|
| 20 |
Efficient uncertainty quantification for a hypersonic trailing-edge flap, using gradient-enhanced kriging
|
Bhattrai, Sudip
|
|
2018
|
80 |
C |
p. 261-268
|
artikel
|
| 21 |
Ethylene flame-holding in double ramp flows
|
Chang, Eric Won Keun
|
|
2018
|
80 |
C |
p. 413-423
|
artikel
|
| 22 |
Extendable chord for improved helicopter rotor performance
|
Han, Dong
|
|
2018
|
80 |
C |
p. 445-451
|
artikel
|
| 23 |
Fuzzy adaptive non-affine attitude tracking control for a generic hypersonic flight vehicle
|
Wang, Yuhui
|
|
2018
|
80 |
C |
p. 56-66
|
artikel
|
| 24 |
Heavy rain effects on aircraft lateral/directional stability and control determined from numerical simulation data
|
Wu, Zhenlong
|
|
2018
|
80 |
C |
p. 472-481
|
artikel
|
| 25 |
Influence of blade lean together with blade clocking on the overall aerodynamic performance of a multi-stage turbine
|
Zhu, Yalu
|
|
2018
|
80 |
C |
p. 329-336
|
artikel
|
| 26 |
Intelligent GNSS/INS integrated navigation system for a commercial UAV flight control system
|
Zhang, Guohao
|
|
2018
|
80 |
C |
p. 368-380
|
artikel
|
| 27 |
Investigation of performance and mode transition in a variable divergence ratio dual-mode combustor
|
Zhang, Chenlin
|
|
2018
|
80 |
C |
p. 496-507
|
artikel
|
| 28 |
LPV gain-scheduled attitude control for satellite with time-varying inertia
|
Jin, Rongyu
|
|
2018
|
80 |
C |
p. 424-432
|
artikel
|
| 29 |
Nonlinear gain-scheduled flight controller design via stable manifold method
|
Tran, Anh Tuan
|
|
2018
|
80 |
C |
p. 301-308
|
artikel
|
| 30 |
Novel HW mixed zig-zag theory accounting for transverse normal deformability and lower-order counterparts assessed by old and new elastostatic benchmarks
|
Icardi, Ugo
|
|
2018
|
80 |
C |
p. 541-571
|
artikel
|
| 31 |
Numerical evaluation of station-keeping strategies for stratospheric balloons
|
Ramesh, Sai Sudha
|
|
2018
|
80 |
C |
p. 288-300
|
artikel
|
| 32 |
Numerical investigations on stator hub initiated stall in a single-stage transonic axial compressor
|
Hu, Jiaguo
|
|
2018
|
80 |
C |
p. 144-155
|
artikel
|
| 33 |
Numerical study on lateral jet interaction in supersonic crossflows
|
Huh, Jinbum
|
|
2018
|
80 |
C |
p. 315-328
|
artikel
|
| 34 |
Online system identification of mini cropped delta UAVs using flight test methods
|
Saderla, Subrahmanyam
|
|
2018
|
80 |
C |
p. 337-353
|
artikel
|
| 35 |
Overview and application of FEM methods for shock analysis in space instruments
|
García-Pérez, Andrés
|
|
2018
|
80 |
C |
p. 572-586
|
artikel
|
| 36 |
Robust two-stage rank filter for Mars entry navigation under parameter uncertainties
|
Zhang, Yongbo
|
|
2018
|
80 |
C |
p. 78-90
|
artikel
|
| 37 |
Rotorcraft comprehensive code assessment for blade–vortex interaction conditions
|
Gennaretti, Massimo
|
|
2018
|
80 |
C |
p. 232-246
|
artikel
|
| 38 |
Sequential multidisciplinary design optimization and reliability analysis under interval uncertainty
|
Wang, Lei
|
|
2018
|
80 |
C |
p. 508-519
|
artikel
|
| 39 |
Study of boundary layer transition on supercritical natural laminar flow wing at high Reynolds number through wind tunnel experiment
|
Xu, Jiakuan
|
|
2018
|
80 |
C |
p. 221-231
|
artikel
|
| 40 |
Switched propulsion force libration control for the low-thrust space tug system
|
Sun, Xin
|
|
2018
|
80 |
C |
p. 281-287
|
artikel
|
| 41 |
Synthesis of attitude control for statically unstable hypersonic vehicle with low-frequency aero-servo-elastic effect
|
Piao, Minnan
|
|
2018
|
80 |
C |
p. 67-77
|
artikel
|
| 42 |
Technology and opportunities of photon sieve CubeSat with deployable optical membrane
|
Kim, Hyun Jung
|
|
2018
|
80 |
C |
p. 212-220
|
artikel
|
| 43 |
The influence of boundaries on sound insulation of the multilayered aerospace poroelastic composite structure
|
Talebitooti, R.
|
|
2018
|
80 |
C |
p. 452-471
|
artikel
|
| 44 |
The optimization and flow diagnoses for a transonic fan with stage flow condition
|
Chen, Huanlong
|
|
2018
|
80 |
C |
p. 247-260
|
artikel
|
| 45 |
Three-dimensional cooperative guidance and control law for multiple reentry missiles with time-varying velocities
|
Wang, Xiaofang
|
|
2018
|
80 |
C |
p. 127-143
|
artikel
|
| 46 |
Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint
|
Guo, Yuyan
|
|
2018
|
80 |
C |
p. 11-19
|
artikel
|
| 47 |
Unsteady aerodynamic model of flexible flapping wing
|
Chen, Si
|
|
2018
|
80 |
C |
p. 354-367
|
artikel
|
| 48 |
Verification and application of a mean flow perturbation method for jet noise
|
Bhaumik, Swagata
|
|
2018
|
80 |
C |
p. 520-540
|
artikel
|
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