| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A computational framework for energy absorption and damage assessment of laminated composites under ballistic impact and new insights into target parameters
|
Goda, Ibrahim
|
|
|
115 |
C |
p.
|
artikel
|
| 2 |
Adaptive super-twisting trajectory tracking control for an unmanned aerial vehicle under gust winds
|
Cui, Lei
|
|
|
115 |
C |
p.
|
artikel
|
| 3 |
Aerodynamic analysis and design optimization of a centrifugal compressor impeller considering realistic manufacturing uncertainties
|
Ju, Yaping
|
|
|
115 |
C |
p.
|
artikel
|
| 4 |
Aircraft turbulence and gust identification using simulated in-flight data
|
Balatti, Davide
|
|
|
115 |
C |
p.
|
artikel
|
| 5 |
An optimal task management and control scheme for military operations with dynamic game strategy
|
Zhang, Tao
|
|
|
115 |
C |
p.
|
artikel
|
| 6 |
Anti-saturation adaptive finite-time neural network based fault-tolerant tracking control for a quadrotor UAV with external disturbances
|
Liu, Kang
|
|
|
115 |
C |
p.
|
artikel
|
| 7 |
A study of the effect of airfoil thickness on the tonal noise generation of finite, wall-mounted airfoils
|
Geyer, Thomas F.
|
|
|
115 |
C |
p.
|
artikel
|
| 8 |
Buzz characteristics and separation bubble dynamics in supersonic intake
|
K James, Jintu
|
|
|
115 |
C |
p.
|
artikel
|
| 9 |
Cascade ensemble-RBF-based optimization algorithm for aero-engine transient control schedule design optimization
|
Ye, Y.
|
|
|
115 |
C |
p.
|
artikel
|
| 10 |
Collision-geometry-based optimal guidance for high-speed target
|
Kim, Boseok
|
|
|
115 |
C |
p.
|
artikel
|
| 11 |
Computational and experimental investigation of ignition in a Mach 2 cavity-based flameholder
|
Hassan, Ez
|
|
|
115 |
C |
p.
|
artikel
|
| 12 |
Coupled investigation on drag reduction and thermal protection mechanism of a double-cone missile by the combined spike and multi-jet
|
Meng, Yu-shan
|
|
|
115 |
C |
p.
|
artikel
|
| 13 |
Design and characterization of a multifunctional low-speed anechoic wind tunnel at HKUST
|
Yi, Wei
|
|
|
115 |
C |
p.
|
artikel
|
| 14 |
Design and performance analysis of a vane shaped rotating receiver hole in high radius pre-swirl systems for gas turbine cooling
|
Liu, Yuxin
|
|
|
115 |
C |
p.
|
artikel
|
| 15 |
Designing trajectories resilient to missed thrust events using expected thrust fraction
|
Rubinsztejn, Ari
|
|
|
115 |
C |
p.
|
artikel
|
| 16 |
Design optimization of velocity-controlled cruise vehicle propelled by throttleable hybrid rocket motor
|
Xiao, Mingyang
|
|
|
115 |
C |
p.
|
artikel
|
| 17 |
Editorial Board
|
|
|
|
115 |
C |
p.
|
artikel
|
| 18 |
Effect of casing treatment to switch the type of instability inception in a high-speed axial compressor
|
Pan, Tianyu
|
|
|
115 |
C |
p.
|
artikel
|
| 19 |
Effects of baffle designs on damping acoustic oscillations in a solid rocket motor
|
Han, Lei
|
|
|
115 |
C |
p.
|
artikel
|
| 20 |
Effects of the foam metal casing treatment on aerodynamic stability and aerocoustic noise in an axial flow compressor
|
Sun, Dakun
|
|
|
115 |
C |
p.
|
artikel
|
| 21 |
Elastic-plastic buckling analysis of stiffened panel subjected to global bending in forming process
|
Zhou, Wenbin
|
|
|
115 |
C |
p.
|
artikel
|
| 22 |
Enhanced adaptive mesh refinement method using advanced vortex identification sensors in wake flow
|
Pang, Chao
|
|
|
115 |
C |
p.
|
artikel
|
| 23 |
Enhancement of ethylene-air continuous rotating detonation in the cavity-based annular combustor
|
Peng, Hao-Yang
|
|
|
115 |
C |
p.
|
artikel
|
| 24 |
Experimental study of a helicopter model in shipboard operations
|
Taymourtash, Neda
|
|
|
115 |
C |
p.
|
artikel
|
| 25 |
Experimental study of the effect of the spray cone angle on the temperature distribution in a can micro-combustor
|
Kankashvar, Benyamin
|
|
|
115 |
C |
p.
|
artikel
|
| 26 |
Experimental study on the collision behaviors of micron-sized aluminum droplets with solid wall in high temperature burned gas
|
Ma, Zhiwei
|
|
|
115 |
C |
p.
|
artikel
|
| 27 |
Impact time constrained integrated guidance and control design
|
Sinha, Abhinav
|
|
|
115 |
C |
p.
|
artikel
|
| 28 |
Improvement in the spring analogy mesh deformation method through the cell-center concept
|
Yang, Yosheph
|
|
|
115 |
C |
p.
|
artikel
|
| 29 |
In-plane compression behaviors of the auxetic star honeycomb: Experimental and numerical simulation
|
Wei, Lulu
|
|
|
115 |
C |
p.
|
artikel
|
| 30 |
Interaction of the wakes of two flapping wings on control forces and moment
|
Han, Jong-Seob
|
|
|
115 |
C |
p.
|
artikel
|
| 31 |
Investigation of local unstart in a hypersonic scramjet intake at a Mach number of 6
|
Devaraj, Manoj Kumar K
|
|
|
115 |
C |
p.
|
artikel
|
| 32 |
Investigations on high-fidelity low-dissipation scheme for unsteady turbulent separated flows
|
Chen, Shu-sheng
|
|
|
115 |
C |
p.
|
artikel
|
| 33 |
Life cycle gas path performance monitoring with control loop parameters uncertainty for aeroengine
|
Jin, Peng
|
|
|
115 |
C |
p.
|
artikel
|
| 34 |
Linear and nonlinear vibrations of graphene platelet reinforced composite tapered plates and cylindrical panels
|
Niu, Yan
|
|
|
115 |
C |
p.
|
artikel
|
| 35 |
Long-term degradation prediction and assessment with heteroscedasticity telemetry data based on GRU-GARCH and MD hybrid method: An application for satellite
|
Tao, Laifa
|
|
|
115 |
C |
p.
|
artikel
|
| 36 |
Mid-fidelity approach to aerodynamic simulations of unconventional VTOL aircraft configurations
|
Tugnoli, Matteo
|
|
|
115 |
C |
p.
|
artikel
|
| 37 |
Mission-oriented performance assessment and optimization of electric multirotors
|
Lim, Daejin
|
|
|
115 |
C |
p.
|
artikel
|
| 38 |
Motion modeling and state estimation in range-Doppler plane
|
Zhou, Gongjian
|
|
|
115 |
C |
p.
|
artikel
|
| 39 |
Noise control for high-lift devices by slat wall treatment
|
Chen, Guoyong
|
|
|
115 |
C |
p.
|
artikel
|
| 40 |
Nonlinear vibration behavior of CNTRC plate with different distribution of CNTs under hygrothermal effects
|
Tang, Hong
|
|
|
115 |
C |
p.
|
artikel
|
| 41 |
Nonsingular impact time guidance and control using deviated pursuit
|
Sinha, Abhinav
|
|
|
115 |
C |
p.
|
artikel
|
| 42 |
Novel optical heating rate measurement in hypersonic flow using phenol formaldehyde luminescence
|
Gonzales, Joseph
|
|
|
115 |
C |
p.
|
artikel
|
| 43 |
Numerical investigation and optimization for interior duct shape of ducted tail rotor
|
Cao, Chenkai
|
|
|
115 |
C |
p.
|
artikel
|
| 44 |
Numerical investigation of real-gas effect of inward-turning inlet at Mach 12
|
Dai, Chunliang
|
|
|
115 |
C |
p.
|
artikel
|
| 45 |
Numerical investigation on the forced vibration induced by the low engine order under boundary layer ingestion condition
|
Pan, Tianyu
|
|
|
115 |
C |
p.
|
artikel
|
| 46 |
Numerical study on the biomimetic trailing edge in the environment of a high-pressure turbine stage
|
Luo, Yuxi
|
|
|
115 |
C |
p.
|
artikel
|
| 47 |
On the application of artificial neural network for the development of a nonlinear aeroelastic model
|
Torregrosa, A.J.
|
|
|
115 |
C |
p.
|
artikel
|
| 48 |
On the dynamic response of a hingeless helicopter rotor blade
|
Sarker, Pratik
|
|
|
115 |
C |
p.
|
artikel
|
| 49 |
Reduction of surface friction drag in scramjet engine by boundary layer combustion
|
Xue, Rui
|
|
|
115 |
C |
p.
|
artikel
|
| 50 |
Reliability analysis for stall warning methods in an axial flow compressor
|
Liu, Yang
|
|
|
115 |
C |
p.
|
artikel
|
| 51 |
Research on the ground vortex and inlet flow field under the ground crosswind condition
|
Chen, Jingjing
|
|
|
115 |
C |
p.
|
artikel
|
| 52 |
Responses and suppression of Joined-Wing UAV in wind field based on distributed model and active disturbance rejection control
|
Wang, Rui
|
|
|
115 |
C |
p.
|
artikel
|
| 53 |
Robust control design based aircraft flat-spin recovery using optimally deflected novel deployable fin
|
Salahudden,
|
|
|
115 |
C |
p.
|
artikel
|
| 54 |
Role of overdriven state of ignition wave in pre-detonators on detonation transition modes in a flat chamber
|
Lei, Qingchun
|
|
|
115 |
C |
p.
|
artikel
|
| 55 |
Simulating unsteady flows in a compressor using immersed boundary method with turbulent wall model
|
Chen, Congcong
|
|
|
115 |
C |
p.
|
artikel
|
| 56 |
Single segment approach and landing guidance and control for an unpowered reusable launch vehicle
|
S. Hameed, Aysha
|
|
|
115 |
C |
p.
|
artikel
|
| 57 |
The aerodynamic characteristics and its estimation method of finned missile experiencing spin-deformation coupling motion
|
Yin, Jintao
|
|
|
115 |
C |
p.
|
artikel
|
| 58 |
The balanced mode decomposition algorithm for data-driven LPV low-order models of aeroservoelastic systems
|
Iannelli, Andrea
|
|
|
115 |
C |
p.
|
artikel
|
| 59 |
The initial flow structures and oscillations of an underexpanded impinging jet
|
Cui, Wei
|
|
|
115 |
C |
p.
|
artikel
|
| 60 |
The role of radial secondary flow in the process of rotating stall for a 1.5-stage axial compressor
|
Li, Hefei
|
|
|
115 |
C |
p.
|
artikel
|
| 61 |
Three-dimensional suboptimal nonlinear impact time guidance against non-maneuvering target
|
Nanavati, Rohit V.
|
|
|
115 |
C |
p.
|
artikel
|
| 62 |
Transient aerodynamic performances and pressure oscillations of a core engine combustor during start up
|
Qin, Hao
|
|
|
115 |
C |
p.
|
artikel
|
| 63 |
Unsteady aero-elastic analysis of a composite wing containing an edge crack
|
Torabi, A.R.
|
|
|
115 |
C |
p.
|
artikel
|
Tijdschrift beschrijving