| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A coupled free-wake/panel method for rotor/fuselage/empennage aerodynamic interaction and helicopter trims
|
Cao, Yihua
|
|
2015
|
|
3 |
p. 435-444
|
artikel
|
| 2 |
Acoustic characterisation of a rectangular rocket combustor with liquid oxygen and hydrogen propellants
|
Hardi, Justin S
|
|
2013
|
|
3 |
p. 436-446
|
artikel
|
| 3 |
Active disturbance rejection guidance and control scheme for homing missiles with impact angle constraints
|
Wang, Jian Hua
|
|
2019
|
|
3 |
p. 1133-1146
|
artikel
|
| 4 |
Adaptive constraint backstepping fault-tolerant control for small carrier-based unmanned aerial vehicle with uncertain parameters
|
Zheng, Feng-ying
|
|
2016
|
|
3 |
p. 407-425
|
artikel
|
| 5 |
Aerodynamic optimization method based on Bezier curve and radial basis function
|
Yang, Fan
|
|
2018
|
|
3 |
p. 459-471
|
artikel
|
| 6 |
Aeroelastic analysis of parachute deceleration systems with empirical aerodynamics
|
Ortega, Enrique
|
|
|
|
3 |
p. 729-741
|
artikel
|
| 7 |
A fault-tolerant control scheme within adaptive disturbance observer for hypersonic vehicle
|
Zhou, Jun
|
|
2019
|
|
3 |
p. 1071-1088
|
artikel
|
| 8 |
A fully autonomous unmanned aerial vehicle landing controller synthesis: quantitative feedback theory and H∞ technique comparison
|
López, J
|
|
2012
|
|
3 |
p. 281-293
|
artikel
|
| 9 |
Analysis of partial wing damage on flying-wing unmanned air vehicle
|
Kim, Ki-joon
|
|
2014
|
|
3 |
p. 355-374
|
artikel
|
| 10 |
Analytical investigation into the effects of nitrogen enriched air bubbles to improve aircraft fuel system water management
|
Terada, Yuri
|
|
2019
|
|
3 |
p. 861-870
|
artikel
|
| 11 |
Analytic and computational analysis of wing twist to minimize induced drag during roll
|
Hunsaker, Douglas F
|
|
|
|
3 |
p. 788-803
|
artikel
|
| 12 |
A new pipe routing method for aero-engines based on genetic algorithm
|
Ren, Tao
|
|
2014
|
|
3 |
p. 424-434
|
artikel
|
| 13 |
An improved decentralized model for sensor fault detection and isolation demonstrated on an airplane system
|
Wang, Jianchen
|
|
2015
|
|
3 |
p. 423-434
|
artikel
|
| 14 |
An integrated approach to vehicle and subsystem sizing and analysis for novel subsystem architectures
|
Chakraborty, Imon
|
|
2016
|
|
3 |
p. 496-514
|
artikel
|
| 15 |
A novel surrogate-based aerodynamic optimization method using field approximate model
|
Wang, Wenjie
|
|
2019
|
|
3 |
p. 883-895
|
artikel
|
| 16 |
Application of a diagnostic technique for evaluating the quality of the air–fuel mixture and the ignition quality of a spark-ignition reciprocating aircraft piston engine
|
Antonopoulos, AK
|
|
2018
|
|
3 |
p. 571-582
|
artikel
|
| 17 |
A semi-analytical solution to the global navigation satellite system attitude determination problem
|
Li, Shengquan
|
|
2019
|
|
3 |
p. 1033-1046
|
artikel
|
| 18 |
A three-dimensional computational study of the effect of the inlet conditions on supersonic mixing and combustion
|
Abdel-Salam, Tarek M
|
|
2013
|
|
3 |
p. 425-435
|
artikel
|
| 19 |
Attitude control design for reusable launch vehicles using adaptive fuzzy control with compensation controller
|
Mao, Qi
|
|
2019
|
|
3 |
p. 823-836
|
artikel
|
| 20 |
Attitude control of a small-scale helicopter based on backstepping
|
Tang, Shuai
|
|
2015
|
|
3 |
p. 502-516
|
artikel
|
| 21 |
Automated optimal flight planning based on the aircraft intent description language
|
González-Arribas, Daniel
|
|
2019
|
|
3 |
p. 928-948
|
artikel
|
| 22 |
Autonomous obstacle avoidance maneuvering of thrust-vectored airship with neural network control
|
Mishra, Amardeep
|
|
|
|
3 |
p. 689-708
|
artikel
|
| 23 |
Axial flow development characteristics of circular and triangular supersonic jets in the presence of an annular coflow at large separation distance
|
Sureshkumar, A
|
|
|
|
3 |
p. 804-817
|
artikel
|
| 24 |
Characteristics of liquid film on the tip surface of indium field-emission electric propulsion thrusters
|
Guo, Dengshuai
|
|
2019
|
|
3 |
p. 908-915
|
artikel
|
| 25 |
Control of a small helicopter with linear matrix inequality-based design assuring stability and performance
|
Şahin, İsmail Hakkı
|
|
|
|
3 |
p. 624-639
|
artikel
|
| 26 |
Design and analysis of an integrated device for launch adapter and resettable orbital deployer for picosatellites
|
Wang, Wenlong
|
|
|
|
3 |
p. 818-826
|
artikel
|
| 27 |
Design and qualification of a supersonic wind tunnel for induced boundary layer transition research
|
Bottini, H
|
|
2015
|
|
3 |
p. 562-578
|
artikel
|
| 28 |
Design of iron bird for a regional jet aircraft
|
Li, Dawei
|
|
|
|
3 |
p. 681-688
|
artikel
|
| 29 |
Determination of optimum specific thrust for civil aero gas turbine engines: a multidisciplinary design synthesis and optimisation
|
Guha, Abhijit
|
|
2013
|
|
3 |
p. 502-527
|
artikel
|
| 30 |
Development of a new conceptual design methodology for parallel hybrid aircraft
|
Boggero, Luca
|
|
2019
|
|
3 |
p. 1047-1058
|
artikel
|
| 31 |
Discharge hollow cathode design for a dual-stage gridded ion engine
|
Coletti, M
|
|
2012
|
|
3 |
p. 272-280
|
artikel
|
| 32 |
Disturbance observer-based sliding manifold predictive control for reentry hypersonic vehicles with multi-constraint
|
Zhang, Jun
|
|
2016
|
|
3 |
p. 485-495
|
artikel
|
| 33 |
Dual-quaternion-based finite-time control for spacecraft tracking in six degrees of freedom
|
Wang, Jianying
|
|
2013
|
|
3 |
p. 528-545
|
artikel
|
| 34 |
Dynamic characteristics analysis of a dual-rotor system with inter-shaft bearing
|
Wang, Nanfei
|
|
2019
|
|
3 |
p. 1147-1158
|
artikel
|
| 35 |
Dynamic cloud back-propagation networks and its application in fault diagnostic for liquid-propellant rocket engines
|
Nie, Yao
|
|
2018
|
|
3 |
p. 583-594
|
artikel
|
| 36 |
Effect of propeller-induced flow on the performance of biplane micro air vehicle dynamics
|
Jana, Shuvrangshu
|
|
|
|
3 |
p. 716-728
|
artikel
|
| 37 |
Effect of viscosity on a propagation of strong compression wave in a cylindrical duct with damping device
|
Vlasenko, Vladimir
|
|
2013
|
|
3 |
p. 493-501
|
artikel
|
| 38 |
Effects of tip clearance size on the unsteady flow behaviors and performance in a counter-rotating axial flow compressor
|
Mao, Xiaochen
|
|
2019
|
|
3 |
p. 1059-1070
|
artikel
|
| 39 |
Electrical load-sizing methodology to aid conceptual and preliminary design of large commercial aircraft
|
Seresinhe, Ravinka
|
|
2015
|
|
3 |
p. 445-466
|
artikel
|
| 40 |
Electric sail-based displaced orbits with a refined thrust model
|
Niccolai, Lorenzo
|
|
2018
|
|
3 |
p. 423-432
|
artikel
|
| 41 |
Energy-aware path planning of an unmanned aerial vehicle acting as a communication relay for mobile ground nodes
|
Choi, Dae H
|
|
2019
|
|
3 |
p. 1124-1132
|
artikel
|
| 42 |
Estimation models for the preliminary design of electromechanical actuators
|
Budinger, M
|
|
2012
|
|
3 |
p. 243-259
|
artikel
|
| 43 |
European Space Agency intermediate experimental vehicle: Development of an independent aerothermodynamic database tool
|
Di Benedetto, Sara
|
|
2014
|
|
3 |
p. 435-454
|
artikel
|
| 44 |
Experimental analysis of cell pattern on grid fin aerodynamics in subsonic flow
|
Tripathi, Manish
|
|
|
|
3 |
p. 537-562
|
artikel
|
| 45 |
Experimental and numerical investigation into the wake of a supercritical airfoil in a compressible unsteady flow
|
Beheshti Boroumand, B
|
|
2017
|
|
3 |
p. 419-434
|
artikel
|
| 46 |
Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle
|
Wang, Yang-Sheng
|
|
|
|
3 |
p. 563-572
|
artikel
|
| 47 |
Experimental and numerical investigations on an airfoil with triangular- and star-shaped damage
|
Etemadi, F
|
|
2012
|
|
3 |
p. 341-360
|
artikel
|
| 48 |
Experimental investigation of the expansion characteristics of vaporized kerosene jets in a quiescent atmospheric environment
|
Yang, Kai
|
|
|
|
3 |
p. 896-907
|
artikel
|
| 49 |
Experimental investigation on the alternate coating method for aircraft anti-icing applications
|
Rose, Bruce Ralphin
|
|
2017
|
|
3 |
p. 407-418
|
artikel
|
| 50 |
Experimental study on the effect of air throttling on supersonic combustion
|
Tian, Ye
|
|
2018
|
|
3 |
p. 472-480
|
artikel
|
| 51 |
Fast fault estimation for linear systems with unmatched faults
|
Li, Fei
|
|
2016
|
|
3 |
p. 554-565
|
artikel
|
| 52 |
Fault-tolerant control for multiple networked spacecraft under actuator saturation
|
Dong, Ning
|
|
2017
|
|
3 |
p. 558-569
|
artikel
|
| 53 |
Flight control clearance of the Cessna Citation X using evolutionary algorithms
|
Boughari, Yamina
|
|
2017
|
|
3 |
p. 510-532
|
artikel
|
| 54 |
Flight mechanics of a novel guided spin-stabilized projectile concept
|
Fresconi, F
|
|
2012
|
|
3 |
p. 327-340
|
artikel
|
| 55 |
Flutter suppression of an aircraft wing with a flexibly mounted mass using magneto-rheological damper
|
Ghasemikaram, Amir Hossein
|
|
|
|
3 |
p. 827-839
|
artikel
|
| 56 |
Fusing unscented Kalman filter for performance monitoring and fault accommodation in gas turbine
|
Lu, Feng
|
|
2018
|
|
3 |
p. 556-570
|
artikel
|
| 57 |
Geometrically exact vortex lattice and panel methods in static aeroelasticity of very flexible wing
|
Yang, Lan
|
|
|
|
3 |
p. 742-759
|
artikel
|
| 58 |
Guidance, navigation and control for autonomous R-bar proximity operations for geostationary satellites
|
Wen, Changxuan
|
|
2017
|
|
3 |
p. 452-473
|
artikel
|
| 59 |
Helicopter flight simulation trim in the coordinated turn with the hybrid genetic algorithm
|
Wang, Wei
|
|
2019
|
|
3 |
p. 1159-1168
|
artikel
|
| 60 |
Helicopter fuselage aerodynamic data fitting using multivariate smoothing thin plate splines
|
Venturelli, Giovanni
|
|
2014
|
|
3 |
p. 384-397
|
artikel
|
| 61 |
Helicopter gas turbine engine performance analysis: A multivariable approach
|
Arush, Ilan
|
|
2019
|
|
3 |
p. 837-850
|
artikel
|
| 62 |
High altitude low Reynolds number effect on the matching performance of a turbofan engine
|
Tang, Hai-Long
|
|
2013
|
|
3 |
p. 455-466
|
artikel
|
| 63 |
Higher harmonic pitch link loads reduction using fluidlastic isolators
|
Han, Dong
|
|
2014
|
|
3 |
p. 455-469
|
artikel
|
| 64 |
Impact time control guidance with field-of-view constraint accounting for uncertain system lag
|
Zhang, Youan
|
|
2016
|
|
3 |
p. 515-529
|
artikel
|
| 65 |
Influence of aeroelastic control reversal problem in the airplane lateral stability modes
|
Rose, J Bruce Ralphin
|
|
2015
|
|
3 |
p. 517-533
|
artikel
|
| 66 |
Influence of wing span on the aerodynamics of wings in ground effect
|
Diasinos, Sammy
|
|
2013
|
|
3 |
p. 569-573
|
artikel
|
| 67 |
Interaction mechanism between shock waves and supersonic film cooling with cracking reaction
|
Zuo, Jingying
|
|
|
|
3 |
p. 908-923
|
artikel
|
| 68 |
Investigation of computational flow fields and aeroacoustic characteristics over a re-entry command module
|
Rose, J Bruce Ralphin
|
|
2018
|
|
3 |
p. 532-544
|
artikel
|
| 69 |
Investigation on application of high-lift configuration to wing-in-ground effect
|
Yang, W
|
|
2012
|
|
3 |
p. 260-271
|
artikel
|
| 70 |
Investigation on metal diaphragm of pulse separation device in dual-pulse solid rocket motor
|
Chunguang, Wang
|
|
2017
|
|
3 |
p. 444-451
|
artikel
|
| 71 |
Key aspects of electric vertical take-off and landing conceptual design
|
Bacchini, Alessandro
|
|
|
|
3 |
p. 774-787
|
artikel
|
| 72 |
Large eddy simulation of the influence of synthetic inlet turbulence on a practical aeroengine combustor with counter-rotating swirler
|
Zhou, Yu
|
|
2019
|
|
3 |
p. 978-990
|
artikel
|
| 73 |
Leakage analysis and ground tests of the O-type rubber ring seal applied in lunar sample return devices
|
Zhang, Bin
|
|
2015
|
|
3 |
p. 479-491
|
artikel
|
| 74 |
Longitudinal automatic carrier landing system guidance law using model predictive control with an additional landing risk term
|
Wang, Lipeng
|
|
2019
|
|
3 |
p. 1089-1105
|
artikel
|
| 75 |
Low observability trajectory planning for stealth aircraft to evade radars tracking
|
Liu, Hongfu
|
|
2014
|
|
3 |
p. 398-410
|
artikel
|
| 76 |
Manipulation strategy of tilt quad rotor based on active disturbance rejection control
|
Wang, Zhigang
|
|
|
|
3 |
p. 573-584
|
artikel
|
| 77 |
Mass properties identification and automatic mass balancing system for satellite attitude dynamics simulator
|
Sharifi, Ghasem
|
|
2019
|
|
3 |
p. 896-907
|
artikel
|
| 78 |
Measurements of water film thickness on a wing surface in simulated heavy rain
|
Wu, Zhenlong
|
|
2016
|
|
3 |
p. 530-538
|
artikel
|
| 79 |
Microvibration suppression of space truss structures using viscoelastic dampers with design parameter optimization
|
Xu, Rui
|
|
2016
|
|
3 |
p. 539-553
|
artikel
|
| 80 |
Multiloop state-dependent nonlinear time-varying sliding mode control of unmanned small-scale helicopter
|
Ozcan, Sinan
|
|
|
|
3 |
p. 585-606
|
artikel
|
| 81 |
Multi-UAVs formation autopilot design and performance analysis under interconnection topologies
|
Yang, Aolei
|
|
2016
|
|
3 |
p. 469-484
|
artikel
|
| 82 |
Natural laminar flow airfoil shape design at transonic regimes with multi-objective evolutionary algorithms
|
Chen, Yongbin
|
|
2019
|
|
3 |
p. 991-999
|
artikel
|
| 83 |
New slip boundary condition in high-speed rarefied gas flow simulations
|
Le, Nam TP
|
|
|
|
3 |
p. 840-856
|
artikel
|
| 84 |
Nonlinear relative dynamics of Lorentz spacecraft about J2-perturbed orbit
|
Huang, Xu
|
|
2015
|
|
3 |
p. 467-478
|
artikel
|
| 85 |
Numerical investigation of tip clearance size effect on the performance and tip leakage flow in a dual-stage counter-rotating axial compressor
|
Mao, Xiaochen
|
|
2017
|
|
3 |
p. 474-484
|
artikel
|
| 86 |
Numerical simulation and parametric study of a supersonic intake
|
Soltani, Mohammad R
|
|
2013
|
|
3 |
p. 467-479
|
artikel
|
| 87 |
Numerical simulation of axisymmetric supersonic viscous flow over a blunt cone with a diagonal fourth-order finite difference method
|
Rashidi, M M
|
|
2012
|
|
3 |
p. 310-326
|
artikel
|
| 88 |
Numerical simulation of non-stationary propagation of combustion along a duct with supersonic flow of a viscid gas
|
Vlasenko, Vladimir
|
|
2013
|
|
3 |
p. 480-492
|
artikel
|
| 89 |
Numerical simulation of three-dimensional rotor icing in hovering flight
|
Wang, Zhengzhi
|
|
2018
|
|
3 |
p. 545-555
|
artikel
|
| 90 |
Online learning fuzzy vibration control of smart truss structure
|
Xu, Rui
|
|
2017
|
|
3 |
p. 548-557
|
artikel
|
| 91 |
On the effect of operating condition on separated-flow control by nanosecond pulse discharge actuators
|
Du, Hai
|
|
2018
|
|
3 |
p. 505-516
|
artikel
|
| 92 |
Optimal cooperative guidance with guaranteed miss distance in three-body engagement
|
Fang, Feng
|
|
2018
|
|
3 |
p. 492-504
|
artikel
|
| 93 |
Optimization of collision avoidance maneuver planning for cluster satellites in space debris explosion situation
|
Seong, Jae-Dong
|
|
2018
|
|
3 |
p. 407-422
|
artikel
|
| 94 |
Parametric effects in a scramjet engine on the interaction between the air stream and the injection
|
Huang, W
|
|
2012
|
|
3 |
p. 294-309
|
artikel
|
| 95 |
Particle image velocimetry study of the impinging height effect on the overexpanded supersonic impinging free jet of Ma = 1.754. Part 2: detailed velocity distribution
|
Xu, Jinglei
|
|
2013
|
|
3 |
p. 546-554
|
artikel
|
| 96 |
Pilot-model-in-the-loop simulation environment to study large aircraft dynamics
|
Lone, Mohammad M
|
|
2013
|
|
3 |
p. 555-568
|
artikel
|
| 97 |
Polynomial guidance law for impact angle control with a seeker look angle limit
|
Zhiming, Zhou
|
|
|
|
3 |
p. 857-870
|
artikel
|
| 98 |
Pruning operator for minimum deck wind in carrier aircraft launch
|
Zhou, Zeyang
|
|
|
|
3 |
p. 655-664
|
artikel
|
| 99 |
Qualitative phenomenological investigation of the transient temperature gradient during gas turbine's hot section component cooling
|
Tahsini, AM
|
|
|
|
3 |
p. 709-715
|
artikel
|
| 100 |
Reevaluating conceptual design fidelity: An efficient supersonic air vehicle design case
|
Allison, Darcy L
|
|
2016
|
|
3 |
p. 581-598
|
artikel
|
| 101 |
Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control
|
Liu, Xiaodong
|
|
2015
|
|
3 |
p. 554-561
|
artikel
|
| 102 |
Research on the method of suppressing sun and moon's interference on infrared conical earth sensor
|
Xianbin, Hu
|
|
2015
|
|
3 |
p. 399-406
|
artikel
|
| 103 |
Robust adaptive sliding sector control and control allocation of a missile with aerodynamic control surfaces and reaction jets
|
Xu, Biao
|
|
2017
|
|
3 |
p. 397-406
|
artikel
|
| 104 |
Robust dynamic surface sliding mode control for attitude tracking of flexible spacecraft with an extended state observer
|
Zhou, Chengbao
|
|
2017
|
|
3 |
p. 533-547
|
artikel
|
| 105 |
Roll aerodynamic characteristics study of an unmanned aerial vehicle based on circulation control technology
|
Chen, Kun
|
|
2019
|
|
3 |
p. 871-882
|
artikel
|
| 106 |
Scale-model tests of coaxial rotors in water tunnel via particle image velocimetry technique
|
Ma, Yimin
|
|
2016
|
|
3 |
p. 426-443
|
artikel
|
| 107 |
Sea-unammned aerial vehicle takeoff characteristics analysis method based on approximate equilibrium hypothesis
|
Ma, Dongli
|
|
2019
|
|
3 |
p. 916-927
|
artikel
|
| 108 |
Sensor fault diagnosis of gas turbine engines using an integrated scheme based on improved least squares support vector regression
|
Hu, Yu
|
|
|
|
3 |
p. 607-623
|
artikel
|
| 109 |
Shimming effect on the mechanical behaviors of composite assembly structures of aircraft
|
Gao, Guoqiang
|
|
2019
|
|
3 |
p. 851-860
|
artikel
|
| 110 |
Sinusoidal function weighted optimal guidance laws
|
Lee, Chang-Hun
|
|
2015
|
|
3 |
p. 534-542
|
artikel
|
| 111 |
Soft landing control of unmanned powered parafoils in unknown wind environments
|
Luo, Shuzhen
|
|
2019
|
|
3 |
p. 949-968
|
artikel
|
| 112 |
Structural reliability assessment based on low-discrepancy adaptive importance sampling and artificial neural network
|
Zhao, Hailong
|
|
2017
|
|
3 |
p. 497-509
|
artikel
|
| 113 |
Study on aerodynamic optimal super/transonic turbine cascade and its geometry characteristics
|
Ji, Lucheng
|
|
2017
|
|
3 |
p. 435-443
|
artikel
|
| 114 |
Study on low-velocity impact and residual strength at high temperatures of composite laminates
|
Weng, Jingmeng
|
|
2019
|
|
3 |
p. 1106-1123
|
artikel
|
| 115 |
Study on navigation and manual steering strategies in the fly-around phase of teleoperation rendezvous and docking
|
Li, Tao
|
|
2018
|
|
3 |
p. 595-609
|
artikel
|
| 116 |
Supersonic jet control with shifted tabs
|
Maruthupandiyan, K
|
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2018
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