nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Aeroelastic analysis of parachute deceleration systems with empirical aerodynamics
|
Ortega, Enrique |
|
|
234 |
3 |
p. 729-741 |
artikel |
2 |
Analytic and computational analysis of wing twist to minimize induced drag during roll
|
Hunsaker, Douglas F |
|
|
234 |
3 |
p. 788-803 |
artikel |
3 |
Autonomous obstacle avoidance maneuvering of thrust-vectored airship with neural network control
|
Mishra, Amardeep |
|
|
234 |
3 |
p. 689-708 |
artikel |
4 |
Axial flow development characteristics of circular and triangular supersonic jets in the presence of an annular coflow at large separation distance
|
Sureshkumar, A |
|
|
234 |
3 |
p. 804-817 |
artikel |
5 |
Control of a small helicopter with linear matrix inequality-based design assuring stability and performance
|
Şahin, İsmail Hakkı |
|
|
234 |
3 |
p. 624-639 |
artikel |
6 |
Design and analysis of an integrated device for launch adapter and resettable orbital deployer for picosatellites
|
Wang, Wenlong |
|
|
234 |
3 |
p. 818-826 |
artikel |
7 |
Design of iron bird for a regional jet aircraft
|
Li, Dawei |
|
|
234 |
3 |
p. 681-688 |
artikel |
8 |
Effect of propeller-induced flow on the performance of biplane micro air vehicle dynamics
|
Jana, Shuvrangshu |
|
|
234 |
3 |
p. 716-728 |
artikel |
9 |
Experimental analysis of cell pattern on grid fin aerodynamics in subsonic flow
|
Tripathi, Manish |
|
|
234 |
3 |
p. 537-562 |
artikel |
10 |
Experimental and numerical investigation of an axisymmetric divergent dual throat nozzle
|
Wang, Yang-Sheng |
|
|
234 |
3 |
p. 563-572 |
artikel |
11 |
Experimental investigation of the expansion characteristics of vaporized kerosene jets in a quiescent atmospheric environment
|
Yang, Kai |
|
|
234 |
3 |
p. 896-907 |
artikel |
12 |
Flutter suppression of an aircraft wing with a flexibly mounted mass using magneto-rheological damper
|
Ghasemikaram, Amir Hossein |
|
|
234 |
3 |
p. 827-839 |
artikel |
13 |
Geometrically exact vortex lattice and panel methods in static aeroelasticity of very flexible wing
|
Yang, Lan |
|
|
234 |
3 |
p. 742-759 |
artikel |
14 |
Interaction mechanism between shock waves and supersonic film cooling with cracking reaction
|
Zuo, Jingying |
|
|
234 |
3 |
p. 908-923 |
artikel |
15 |
Key aspects of electric vertical take-off and landing conceptual design
|
Bacchini, Alessandro |
|
|
234 |
3 |
p. 774-787 |
artikel |
16 |
Manipulation strategy of tilt quad rotor based on active disturbance rejection control
|
Wang, Zhigang |
|
|
234 |
3 |
p. 573-584 |
artikel |
17 |
Multiloop state-dependent nonlinear time-varying sliding mode control of unmanned small-scale helicopter
|
Ozcan, Sinan |
|
|
234 |
3 |
p. 585-606 |
artikel |
18 |
New slip boundary condition in high-speed rarefied gas flow simulations
|
Le, Nam TP |
|
|
234 |
3 |
p. 840-856 |
artikel |
19 |
Polynomial guidance law for impact angle control with a seeker look angle limit
|
Zhiming, Zhou |
|
|
234 |
3 |
p. 857-870 |
artikel |
20 |
Pruning operator for minimum deck wind in carrier aircraft launch
|
Zhou, Zeyang |
|
|
234 |
3 |
p. 655-664 |
artikel |
21 |
Qualitative phenomenological investigation of the transient temperature gradient during gas turbine's hot section component cooling
|
Tahsini, AM |
|
|
234 |
3 |
p. 709-715 |
artikel |
22 |
Sensor fault diagnosis of gas turbine engines using an integrated scheme based on improved least squares support vector regression
|
Hu, Yu |
|
|
234 |
3 |
p. 607-623 |
artikel |
23 |
Target-bundled genetic algorithm for multi-unmanned aerial vehicle cooperative task assignment considering precedence constraints
|
Xu, Guangtong |
|
|
234 |
3 |
p. 760-773 |
artikel |
24 |
The effect of high temperature steam ingestion on aerodynamic performance and stability of a low-speed axial compressor
|
Tu, Baofeng |
|
|
234 |
3 |
p. 871-886 |
artikel |
25 |
Three-dimensional waypoint following for fixed-wing unmanned aerial vehicles in obstacle-filled environments
|
Singh, Nikhil Kumar |
|
|
234 |
3 |
p. 640-654 |
artikel |
26 |
Transient influence of water injection on the flow field of a hot launch in a W-shaped silo
|
Shi, Shaoyan |
|
|
234 |
3 |
p. 665-680 |
artikel |
27 |
Unmanned aerial vehicle trajectory data fusion based on an active and passive feedback system
|
Tang, Xin-min |
|
|
234 |
3 |
p. 887-895 |
artikel |