| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Acoustic energy absorption and dissipation characteristic of Helmholtz resonator enhanced and broadened by acoustic black hole
|
Zhou, X.Q.
|
|
|
81 |
C |
p. 237-248
|
artikel
|
| 2 |
Airbrake controls of pitching moment and pressure fluctuation for an oblique tail fighter model
|
Cui, Wenyao
|
|
|
81 |
C |
p. 294-305
|
artikel
|
| 3 |
An efficient setup for freestream turbulence on transition prediction over aerospace configurations
|
Halila, Gustavo Luiz Olichevis
|
|
|
81 |
C |
p. 259-271
|
artikel
|
| 4 |
An optimal approach to the preliminary design of small hybrid-electric aircraft
|
Riboldi, Carlo E.D.
|
|
|
81 |
C |
p. 14-31
|
artikel
|
| 5 |
A PCA–ANN-based inverse design model of stall lift robustness for high-lift device
|
Wang, Xinyu
|
|
|
81 |
C |
p. 272-283
|
artikel
|
| 6 |
Application of ICC LPV control to a blended-wing-body airplane with guaranteed H ∞ performance
|
He, Tianyi
|
|
|
81 |
C |
p. 88-98
|
artikel
|
| 7 |
Assessment of dynamic instability of laminated composite-sandwich plates
|
Sahoo, Rosalin
|
|
|
81 |
C |
p. 41-52
|
artikel
|
| 8 |
Automatic carrier landing control for unmanned aerial vehicles based on preview control and particle filtering
|
Zhen, Ziyang
|
|
|
81 |
C |
p. 99-107
|
artikel
|
| 9 |
Decentralized formation flight via PID and integral sliding mode control
|
Thien, Rebbecca T.Y.
|
|
|
81 |
C |
p. 322-332
|
artikel
|
| 10 |
Design of a transonic wing with an adaptive morphing trailing edge via aerostructural optimization
|
Burdette, David A.
|
|
|
81 |
C |
p. 192-203
|
artikel
|
| 11 |
Editorial Board
|
|
|
|
81 |
C |
p. ii
|
artikel
|
| 12 |
Effect of arbitrary yaw/pitch angle in bird strike numerical simulation using SPH method
|
Zhang, Zhuo
|
|
|
81 |
C |
p. 284-293
|
artikel
|
| 13 |
Effect of axisymmetric endwall contouring on the high-load low-reaction transonic compressor rotor with a substantial meridian contraction
|
Sun, Shijun
|
|
|
81 |
C |
p. 78-87
|
artikel
|
| 14 |
Effect of bio-inspired sinusoidal leading-edges on wings
|
Post, Martiqua L.
|
|
|
81 |
C |
p. 128-140
|
artikel
|
| 15 |
Effect of low dorsal fin on the breakdown of vortices over a slender delta wing
|
Meng, Xuanshi
|
|
|
81 |
C |
p. 316-321
|
artikel
|
| 16 |
Experimental characterization of the transonic test section flow in a Ludwieg tube
|
Hammer, B.
|
|
|
81 |
C |
p. 249-258
|
artikel
|
| 17 |
Fractional-order controllers optimized via heterogeneous comprehensive learning pigeon-inspired optimization for autonomous aerial refueling hose–drogue system
|
Sun, Yongbin
|
|
|
81 |
C |
p. 1-13
|
artikel
|
| 18 |
Free vibrations of functionally graded polymer composite nanoplates reinforced with graphene nanoplatelets
|
Arefi, Mohammad
|
|
|
81 |
C |
p. 108-117
|
artikel
|
| 19 |
Influence of thickness on performance characteristics of non-sinusoidal plunging motion of symmetric airfoil
|
Sankarasubramanian, R.
|
|
|
81 |
C |
p. 333-347
|
artikel
|
| 20 |
Interval analysis of the standard of adaptive cycle engine component performance deviation
|
Chen, Min
|
|
|
81 |
C |
p. 179-191
|
artikel
|
| 21 |
Inverse design and Mach 6 experimental investigation of a pressure controllable bump
|
Yu, Zonghan
|
|
|
81 |
C |
p. 204-212
|
artikel
|
| 22 |
Investigation of stall process flow field in transonic centrifugal compressor with volute
|
Yang, Ce
|
|
|
81 |
C |
p. 53-64
|
artikel
|
| 23 |
Nonlinear robust control of tail-sitter aircrafts in flight mode transitions
|
Li, Zhaoying
|
|
|
81 |
C |
p. 348-361
|
artikel
|
| 24 |
Numerical investigation of shock train unsteady movement in a mixing duct
|
Lu, Lei
|
|
|
81 |
C |
p. 375-382
|
artikel
|
| 25 |
Numerical investigations on lifting and flow performance of finger seal with grooved pad
|
Jia, Xingyun
|
|
|
81 |
C |
p. 225-236
|
artikel
|
| 26 |
Operation matching model and analysis between an air inlet and a compressor in an Air Turbo Rocket
|
Liu, Yang
|
|
|
81 |
C |
p. 306-315
|
artikel
|
| 27 |
Performance analysis and path planning for UAVs swarms based on RSS measurements
|
Wang, Weijia
|
|
|
81 |
C |
p. 157-166
|
artikel
|
| 28 |
Performance improvement of variable speed rotors by Gurney flaps
|
Han, Dong
|
|
|
81 |
C |
p. 118-127
|
artikel
|
| 29 |
Plume flowfield and propulsive performance analysis of a rotating detonation engine
|
Sun, Jian
|
|
|
81 |
C |
p. 383-393
|
artikel
|
| 30 |
Position tracking control of a helicopter in ground effect using nonlinear disturbance observer-based incremental backstepping approach
|
Hu, Jinshuo
|
|
|
81 |
C |
p. 167-178
|
artikel
|
| 31 |
Pressure wave damping in transonic airfoil flow by means of micro vortex generators
|
Gageik, M.
|
|
|
81 |
C |
p. 65-77
|
artikel
|
| 32 |
Reset observer design for time-varying dynamics: Application to WIG crafts
|
Aminzadeh, Arash
|
|
|
81 |
C |
p. 32-40
|
artikel
|
| 33 |
Rotating detonation in a ramjet engine three-dimensional modeling
|
Smirnov, N.N.
|
|
|
81 |
C |
p. 213-224
|
artikel
|
| 34 |
Sensitivity assessment of optimal solution in aerodynamic design optimisation using SU2
|
Yang, Guangda
|
|
|
81 |
C |
p. 362-374
|
artikel
|
| 35 |
The crack detection and evaluation by elastic wave propagation in open hole structures for aerospace application
|
Barski, Marek
|
|
|
81 |
C |
p. 141-156
|
artikel
|
Tijdschrift beschrijving