nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A brief review of alternative propellants and requirements for pulsed plasma thrusters in micropropulsion applications
|
LING, William Yeong Liang |
|
|
33 |
12 |
p. 2999-3010 |
artikel |
2 |
Acceleration tracking control for a spinning glide guided projectile with multiple disturbances
|
CHEN, Qi |
|
|
33 |
12 |
p. 3405-3422 |
artikel |
3 |
A constitutive model coupling damage and material anisotropy for wide stress triaxiality
|
LI, Rui |
|
|
33 |
12 |
p. 3509-3525 |
artikel |
4 |
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
|
JIANG, Zonglin |
|
|
33 |
12 |
p. 3027-3038 |
artikel |
5 |
A dynamic modeling approach for nonlinear vibration analysis of the L-type pipeline system with clamps
|
CHAI, Qingdong |
|
|
33 |
12 |
p. 3253-3265 |
artikel |
6 |
An allowance allocation method based on dynamic approximation via online inspection data for deformation control of structural parts
|
HAO, Xiaozhong |
|
|
33 |
12 |
p. 3495-3508 |
artikel |
7 |
An efficient regulation approach for tomographic reconstruction in combustion diagnostics based on TDLAS method
|
XIN, Mingyuan |
|
|
33 |
12 |
p. 3158-3166 |
artikel |
8 |
An enhanced least squares residual RAIM algorithm based on optimal decentralized factor
|
SUN, Guanghui |
|
|
33 |
12 |
p. 3369-3379 |
artikel |
9 |
A review on carrier aircraft dispatch path planning and control on deck
|
WANG, Xinwei |
|
|
33 |
12 |
p. 3039-3057 |
artikel |
10 |
CFD/CSD-based flutter prediction method for experimental models in a transonic wind tunnel with porous wall
|
GUO, Tongqing |
|
|
33 |
12 |
p. 3100-3111 |
artikel |
11 |
Chatter stability and precision during high-speed ultrasonic vibration cutting of a thin-walled titanium cylinder
|
PENG, Zhenlong |
|
|
33 |
12 |
p. 3535-3549 |
artikel |
12 |
Coating deposition regularity depended on orientation difference in PS-PVD plasma jet
|
MAO, Jie |
|
|
33 |
12 |
p. 3460-3468 |
artikel |
13 |
Conceptual design, modeling and compliance characterization of a novel 2-DOF rotational pointing mechanism for fast steering mirror
|
ABID, Muhammad |
|
|
33 |
12 |
p. 3564-3574 |
artikel |
14 |
Coning motion instability of spinning missiles induced by the delay of strap-down seeker
|
HU, Xiao |
|
|
33 |
12 |
p. 3360-3368 |
artikel |
15 |
Coupling plasma plume of a low-power magnetically shielded Hall thruster with a hollow cathode
|
ZHANG, Guangchuan |
|
|
33 |
12 |
p. 3018-3026 |
artikel |
16 |
Deformation behaviors of four-layered U-shaped metallic bellows in hydroforming
|
LIU, Jing |
|
|
33 |
12 |
p. 3479-3494 |
artikel |
17 |
Design and experimental study of a new flapping wing rotor micro aerial vehicle
|
DONG, Xin |
|
|
33 |
12 |
p. 3092-3099 |
artikel |
18 |
Dual smoothing ionospheric gradient monitoring algorithm for dual-frequency BDS GBAS
|
WANG, Zhipeng |
|
|
33 |
12 |
p. 3395-3404 |
artikel |
19 |
Dynamics response analysis of airborne external storage system with clearance between missile-frame
|
YANG, Yongfeng |
|
|
33 |
12 |
p. 3278-3287 |
artikel |
20 |
Editorial Board
|
|
|
|
33 |
12 |
p. ii |
artikel |
21 |
Effects of Mach numbers on Magnus induced surface pressure
|
ASKARY, F. |
|
|
33 |
12 |
p. 3058-3072 |
artikel |
22 |
Evasion guidance algorithms for air-breathing hypersonic vehicles in three-player pursuit-evasion games
|
YAN, Tian |
|
|
33 |
12 |
p. 3423-3436 |
artikel |
23 |
Extension of continuous scanning laser Doppler vibrometry measurement for complex structures with curved surfaces
|
LIU, Cuihong |
|
|
33 |
12 |
p. 3220-3227 |
artikel |
24 |
Gaussian fitting based optimal design of aircraft mission success space using multi-objective genetic algorithm
|
GAO, Yuan |
|
|
33 |
12 |
p. 3318-3330 |
artikel |
25 |
Improved local amplification factor transport equation for stationary crossflow instability in subsonic and transonic flows
|
XU, Jiakuan |
|
|
33 |
12 |
p. 3073-3081 |
artikel |
26 |
Influence mechanism of machining angles on force induced error and their selection in five axis bullnose end milling
|
ZHU, Zerun |
|
|
33 |
12 |
p. 3447-3459 |
artikel |
27 |
Influences of characteristic parameters on starting-up process of an arcjet thruster
|
SHEN, Yan |
|
|
33 |
12 |
p. 3011-3017 |
artikel |
28 |
Inside Front Cover - Aims & Scope, Copyright, Publication information, Orders & Claims, Advertising information, Author inquiries, Permissions, Funding body, Permanence of paper, Impressum (German titles only) and GFA link in double column
|
|
|
|
33 |
12 |
p. IFC |
artikel |
29 |
Intrinsic physical relationships between rotor modal shapes and instantaneous vibrational energy flow transmission characteristics: Theoretical and numerical analysis and application
|
MA, Yingqun |
|
|
33 |
12 |
p. 3288-3305 |
artikel |
30 |
Lightweight hybrid visual-inertial odometry with closed-form zero velocity update
|
QIU, Xiaochen |
|
|
33 |
12 |
p. 3344-3359 |
artikel |
31 |
{MC COMMENT: PA CORRECTION}Theoretical study of ullage washing with mixed inert gas in a non-equilibrium state
|
FENG, Shiyu |
|
|
33 |
12 |
p. 3167-3175 |
artikel |
32 |
Modeling and analysis of solar Doppler difference bias with arbitrary rotation axis
|
LIU, Jin |
|
|
33 |
12 |
p. 3331-3343 |
artikel |
33 |
Modulation of driving signals in flow control over an airfoil with synthetic jet
|
LIU, Zhiyong |
|
|
33 |
12 |
p. 3138-3148 |
artikel |
34 |
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
|
HUANG, Tinglong |
|
|
33 |
12 |
p. 3176-3188 |
artikel |
35 |
Optimization and analysis of winglet configuration for solar aircraft
|
ZHANG, Liang |
|
|
33 |
12 |
p. 3238-3252 |
artikel |
36 |
Physical model for acoustic resonance in annular cavity structure
|
ZHAO, Fengtong |
|
|
33 |
12 |
p. 3228-3237 |
artikel |
37 |
Prediction of pilot workload in helicopter landing after one engine failure
|
YU, Zhiming |
|
|
33 |
12 |
p. 3112-3124 |
artikel |
38 |
Reliability evaluation of avionics system with imperfect fault coverage and propagated failure mechanisms
|
CHEN, Ying |
|
|
33 |
12 |
p. 3437-3446 |
artikel |
39 |
Resistance welding of glass fiber reinforced thermoplastic composite: Experimental investigation and process parameter optimization
|
DU, Bing |
|
|
33 |
12 |
p. 3469-3478 |
artikel |
40 |
Robust fault-tolerant attitude control for satellite with multiple uncertainties and actuator faults
|
FAN, Liming |
|
|
33 |
12 |
p. 3380-3394 |
artikel |
41 |
Semi-analytical model for flat indentation of metal materials and its applications
|
LIU, Xiaokun |
|
|
33 |
12 |
p. 3266-3277 |
artikel |
42 |
Simulation of multi-axis grinding considering runout based on envelope theory
|
JIANG, Yan |
|
|
33 |
12 |
p. 3526-3534 |
artikel |
43 |
Strong interactions of incident shock wave with boundary layer along compression corner
|
GUO, Shanguang |
|
|
33 |
12 |
p. 3149-3157 |
artikel |
44 |
Study of riblet drag reduction for an infinite span wing with different sweep angles
|
ZHANG, Yufei |
|
|
33 |
12 |
p. 3125-3137 |
artikel |
45 |
Team effectiveness evaluation and virtual reality scenario mapping model for helicopter emergency rescue
|
SUN, Xue |
|
|
33 |
12 |
p. 3306-3317 |
artikel |
46 |
Topology optimization in lightweight design of a 3D-printed flapping-wing micro aerial vehicle
|
CHEN, Long |
|
|
33 |
12 |
p. 3206-3219 |
artikel |
47 |
Transient flow characteristics and performance of a solid rocket motor with a pintle valve
|
SONG, Anchen |
|
|
33 |
12 |
p. 3189-3205 |
artikel |
48 |
Water takeoff performance calculation method for amphibious aircraft based on digital virtual flight
|
WANG, Lixin |
|
|
33 |
12 |
p. 3082-3091 |
artikel |
49 |
Whole-process modeling of titanium disc forming for gradient distributions of temperature and deformation
|
LI, Hongwei |
|
|
33 |
12 |
p. 3550-3563 |
artikel |