| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Adjoint aerodynamic optimization of a transonic fan rotor blade with a localized two-level mesh deformation method
|
Tang, Xiao
|
|
|
72 |
C |
p. 267-277
|
artikel
|
| 2 |
Analysis of cooling performance and combustion flow in advanced vortex combustor with guide vane
|
Zeng, Zhuoxiong
|
|
|
72 |
C |
p. 542-552
|
artikel
|
| 3 |
Analytical entry guidance for no-fly-zone avoidance
|
Yu, Wenbin
|
|
|
72 |
C |
p. 426-442
|
artikel
|
| 4 |
An autonomous aerial combat framework for two-on-two engagements based on basic fighter maneuvers
|
Shin, Heemin
|
|
|
72 |
C |
p. 305-315
|
artikel
|
| 5 |
A new approach of casing treatment design for high speed compressors running at partial speeds with low speed large scale test
|
Nan, Xi
|
|
|
72 |
C |
p. 104-113
|
artikel
|
| 6 |
A novel quasi-3D hyperbolic theory for free vibration of FG plates with porosities resting on Winkler/Pasternak/Kerr foundation
|
Shahsavari, Davood
|
|
|
72 |
C |
p. 134-149
|
artikel
|
| 7 |
Anti-disturbance fault tolerant initial alignment for inertial navigation system subjected to multiple disturbances
|
Cao, Songyin
|
|
|
72 |
C |
p. 95-103
|
artikel
|
| 8 |
A port-Hamiltonian framework for operator force assisting systems: Application to the design of helicopter flight controls
|
Touron, Matthieu
|
|
|
72 |
C |
p. 493-501
|
artikel
|
| 9 |
A review of aircraft wing mass estimation methods
|
Dababneh, Odeh
|
|
|
72 |
C |
p. 256-266
|
artikel
|
| 10 |
Assessment methods for unsteady flow distortion in aero-engine intakes
|
Gil-Prieto, Daniel
|
|
|
72 |
C |
p. 292-304
|
artikel
|
| 11 |
Assessment of a hybrid RANS/LES simulation method and URANS method in depicting the unsteady motions of flow structures in a scramjet combustor
|
Han, Yiyu
|
|
|
72 |
C |
p. 114-122
|
artikel
|
| 12 |
Attitude acquisition from an arbitrary tumbling state using two skewed reaction wheels
|
Ousaloo, Hamed Shahmohamadi
|
|
|
72 |
C |
p. 84-94
|
artikel
|
| 13 |
Attitude controller design for reusable launch vehicles during reentry phase via compound adaptive fuzzy H-infinity control
|
Mao, Qi
|
|
|
72 |
C |
p. 36-48
|
artikel
|
| 14 |
Automated Trajectory Optimizer for Solar Sailing (ATOSS)
|
Peloni, Alessandro
|
|
|
72 |
C |
p. 465-475
|
artikel
|
| 15 |
Bay cavity noise for full-scale nose landing gear: A comparison between experimental and numerical results
|
Neri, Eleonora
|
|
|
72 |
C |
p. 278-291
|
artikel
|
| 16 |
Comparison between aerodynamic designs obtained by human driven and automatic procedures
|
Puente, Ricardo
|
|
|
72 |
C |
p. 443-454
|
artikel
|
| 17 |
Continuous momentum management for space station based on LESO
|
Liu, Ping
|
|
|
72 |
C |
p. 364-370
|
artikel
|
| 18 |
Control oriented modeling and analysis of centrifugal compressor working characteristic at variable altitude
|
Zhao, Dongdong
|
|
|
72 |
C |
p. 174-182
|
artikel
|
| 19 |
Control strategy of sideslip perching maneuver under dynamic stall influence
|
Feroskhan, Mir
|
|
|
72 |
C |
p. 150-163
|
artikel
|
| 20 |
Database self-expansion based on artificial neural network: An approach in aircraft design
|
Wang, Shuyue
|
|
|
72 |
C |
p. 77-83
|
artikel
|
| 21 |
Disturbance observer based attitude control for flexible spacecraft with input magnitude and rate constraints
|
Liu, Zhijie
|
|
|
72 |
C |
p. 486-492
|
artikel
|
| 22 |
Dynamic response of vortex breakdown flows to a pitching double-delta wing
|
Liu, Jian
|
|
|
72 |
C |
p. 564-577
|
artikel
|
| 23 |
Editorial Board
|
|
|
|
72 |
C |
p. ii
|
artikel
|
| 24 |
Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor
|
Zhang, Chenlin
|
|
|
72 |
C |
p. 516-524
|
artikel
|
| 25 |
Efficient infinite-swept wing solver for steady and unsteady compressible flows
|
Franciolini, Matteo
|
|
|
72 |
C |
p. 217-229
|
artikel
|
| 26 |
Feedback formation control of UAV swarm with multiple implicit leaders
|
He, Lvlong
|
|
|
72 |
C |
p. 327-334
|
artikel
|
| 27 |
Flow physics and chine control of the water spray generated by an aircraft rigid tire rolling on contaminated runways
|
Zhao, Kaibin
|
|
|
72 |
C |
p. 49-62
|
artikel
|
| 28 |
Flow separation control using unsteady pulsed suction through endwall bleeding holes in a highly loaded compressor cascade
|
Zhang, Hongxin
|
|
|
72 |
C |
p. 455-464
|
artikel
|
| 29 |
Ground effects on the stability of separated flow around a NACA 4415 airfoil at low Reynolds numbers
|
He, Wei
|
|
|
72 |
C |
p. 63-76
|
artikel
|
| 30 |
Hypersonic shock tunnel studies of Edney Type III and IV shock interactions
|
Khatta, Abhishek
|
|
|
72 |
C |
p. 335-352
|
artikel
|
| 31 |
Impact of solar cell characteristics and operating conditions on the sizing of a solar powered nonrigid airship
|
Pande, Durlabh
|
|
|
72 |
C |
p. 353-363
|
artikel
|
| 32 |
Improvement of aerodynamic performance of a low speed axial compressor rotor blade row through air injection
|
Taghavi-Zenouz, Reza
|
|
|
72 |
C |
p. 409-417
|
artikel
|
| 33 |
Investigation on drag reduction performance of aero engine blade with micro-texture
|
Zhang, Chen
|
|
|
72 |
C |
p. 380-396
|
artikel
|
| 34 |
Lift improvements using duty-cycled plasma actuation at low Reynolds numbers
|
Meng, Xuanshi
|
|
|
72 |
C |
p. 123-133
|
artikel
|
| 35 |
Mission optimisation for a conceptual coaxial rotorcraft for taxi applications
|
Enconniere, J.
|
|
|
72 |
C |
p. 14-24
|
artikel
|
| 36 |
Monte Carlo simulation based time limited dispatch analysis with the constraint of dispatch reliability for electronic engine control systems
|
Lu, Zhong
|
|
|
72 |
C |
p. 397-408
|
artikel
|
| 37 |
Numerical research on the effect of variable droop leading-edge on oscillating NACA 0012 airfoil dynamic stall
|
Niu, Jianping
|
|
|
72 |
C |
p. 476-485
|
artikel
|
| 38 |
Numerical simulation of unsteady tip clearance flow in a transonic compressor rotor
|
Wang, Zhiqiang
|
|
|
72 |
C |
p. 193-203
|
artikel
|
| 39 |
Objective quantification of perceived differences between measured and synthesized aircraft sounds
|
Sahai, Abhishek K.
|
|
|
72 |
C |
p. 25-35
|
artikel
|
| 40 |
Onboard mission planning for agile satellite using modified mixed-integer linear programming
|
She, Yuchen
|
|
|
72 |
C |
p. 204-216
|
artikel
|
| 41 |
Power optimization of a single propeller airplane take-off run on the basis of lateral maneuver limitations
|
Stojaković, Predrag
|
|
|
72 |
C |
p. 553-563
|
artikel
|
| 42 |
Preliminary development of an onboard weight and balance estimator for commercial aircraft
|
Chaves, F.A.V.
|
|
|
72 |
C |
p. 316-326
|
artikel
|
| 43 |
Probe motion compound control for autonomous aerial refueling docking
|
Su, Zikang
|
|
|
72 |
C |
p. 1-13
|
artikel
|
| 44 |
Robust Kalman estimators for systems with multiplicative and uncertain-variance linearly correlated additive white noises
|
Liu, Wenqiang
|
|
|
72 |
C |
p. 230-247
|
artikel
|
| 45 |
Rotor airfoil profile optimization for alleviating dynamic stall characteristics
|
Wang, Qing
|
|
|
72 |
C |
p. 502-515
|
artikel
|
| 46 |
Simulation of C-130 H/J troop doors and cargo ramp flow fields
|
Bergeron, Keith
|
|
|
72 |
C |
p. 525-541
|
artikel
|
| 47 |
Spatially and temporally resolved regression rate measurements for the combustion of paraffin wax for hybrid rocket motor applications
|
Dunn, C.
|
|
|
72 |
C |
p. 371-379
|
artikel
|
| 48 |
Stability analysis of a multirotor vehicle hovering condition
|
de Angelis, Emanuele L.
|
|
|
72 |
C |
p. 248-255
|
artikel
|
| 49 |
Unconventional hybrid airships design optimization accounting for added masses
|
Ceruti, A.
|
|
|
72 |
C |
p. 164-173
|
artikel
|
| 50 |
Unstart/restart hysteresis characteristics analysis of an over–under TBCC inlet caused by backpressure and splitter
|
Li, Nan
|
|
|
72 |
C |
p. 418-425
|
artikel
|
| 51 |
Vibration suppression of flexible spacecraft during attitude maneuver using CMGs
|
Guo, Jitang
|
|
|
72 |
C |
p. 183-192
|
artikel
|
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