nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
Advantage of ethanol fuel for gas generator cycle air turbo ramjet engine
|
Minato, Ryojiro |
|
2016 |
50 |
C |
p. 161-172 12 p. |
artikel |
2 |
Aerodynamic design of a MALE UAV
|
Panagiotou, P. |
|
2016 |
50 |
C |
p. 127-138 12 p. |
artikel |
3 |
Aerothermal exploration of reaction control jet in supersonic crossflow at high altitude
|
Chandra Murty, M.S.R. |
|
2016 |
50 |
C |
p. 266-271 6 p. |
artikel |
4 |
Analysis of population damage by space debris upon collision with Earth based on the reverse geocoding method
|
Lee, Mi-hyun |
|
2016 |
50 |
C |
p. 139-148 10 p. |
artikel |
5 |
An assessment of distributed propulsion: Part B – Advanced propulsion system architectures for blended wing body aircraft configurations
|
Kirner, Rudi |
|
2016 |
50 |
C |
p. 212-219 8 p. |
artikel |
6 |
An elastic element of the forced oscillation apparatus for dynamic wind tunnel measurements
|
Samardžić, M. |
|
2016 |
50 |
C |
p. 272-280 9 p. |
artikel |
7 |
An experimental study of high-velocity impact on elastic–plastic crushable polyurethane foams
|
Taherkhani, Ali |
|
2016 |
50 |
C |
p. 245-255 11 p. |
artikel |
8 |
Application of the 3D multi-block CST method to hypersonic aircraft optimization
|
Liu, Chuanzhen |
|
2016 |
50 |
C |
p. 295-303 9 p. |
artikel |
9 |
Convective heat transfer and thermo-diffusion effects on flow of nanofluid towards a permeable stretching sheet saturated by a porous medium
|
Khan, Umar |
|
2016 |
50 |
C |
p. 196-203 8 p. |
artikel |
10 |
Correction method of the manned spacecraft low altitude ranging based on γ ray
|
Liu, Jinglei |
|
2016 |
50 |
C |
p. 71-76 6 p. |
artikel |
11 |
Design and modeling of a novel translational and angular micro-electromechanical accelerometer
|
Amereh, M. |
|
2016 |
50 |
C |
p. 15-24 10 p. |
artikel |
12 |
Dynamics of sideslip perching maneuver under dynamic stall influence
|
Feroskhan, Mir |
|
2016 |
50 |
C |
p. 220-233 14 p. |
artikel |
13 |
Editorial Board
|
|
|
2016 |
50 |
C |
p. IFC- 1 p. |
artikel |
14 |
Effects of combined hardening and free-play nonlinearities on the response of a typical aeroelastic section
|
Pereira, Daniel A. |
|
2016 |
50 |
C |
p. 44-54 11 p. |
artikel |
15 |
Extended State Observer based robust attitude control of spacecraft with input saturation
|
Li, Bo |
|
2016 |
50 |
C |
p. 173-182 10 p. |
artikel |
16 |
Flight formation of UAVs in presence of moving obstacles using fast-dynamic mixed integer linear programming
|
Radmanesh, Mohammadreza |
|
2016 |
50 |
C |
p. 149-160 12 p. |
artikel |
17 |
Further investigation of the body torques on a square solar sail due to the displacement of the sail attachment points
|
Fu, B. |
|
2016 |
50 |
C |
p. 281-294 14 p. |
artikel |
18 |
General analytical models characterizing MBOC modulated signal
|
Zitouni, Sihem |
|
2016 |
50 |
C |
p. 112-126 15 p. |
artikel |
19 |
Hybrid-Trefftz formulation for analysis of thick orthotropic plates
|
Karkon, Mohammad |
|
2016 |
50 |
C |
p. 234-244 11 p. |
artikel |
20 |
Numerical prediction of nozzle flow separation: Issue of turbulence modeling
|
Yaravintelimath, Allamaprabhu |
|
2016 |
50 |
C |
p. 31-43 13 p. |
artikel |
21 |
Numerical study on wall pressure over cone region of blunt-nosed body in high enthalpy shock tunnel HIEST
|
Ishihara, Tomoaki |
|
2016 |
50 |
C |
p. 256-265 10 p. |
artikel |
22 |
Optimal air route flight conflict resolution based on receding horizon control
|
Tang, Xin-Min |
|
2016 |
50 |
C |
p. 77-87 11 p. |
artikel |
23 |
Retrofitting scheme and experimental research of severally damaged carbon fiber reinforced lattice-core sandwich cylinder
|
Wang, Peng |
|
2016 |
50 |
C |
p. 55-61 7 p. |
artikel |
24 |
Robust and optimal control of shimmy vibration in aircraft nose landing gear
|
Tourajizadeh, H. |
|
2016 |
50 |
C |
p. 1-14 14 p. |
artikel |
25 |
Transient probabilistic analysis for turbine blade-tip radial clearance with multi-component and multi-physics fields based on DCERSM
|
Fei, Cheng-Wei |
|
2016 |
50 |
C |
p. 62-70 9 p. |
artikel |
26 |
Transitions in the unsteady wakes and aerodynamic characteristics of the flow past three square cylinders aligned inline
|
Islam, Shams Ul |
|
2016 |
50 |
C |
p. 96-111 16 p. |
artikel |
27 |
Transverse jet in supersonic crossflows
|
Huang, Wei |
|
2016 |
50 |
C |
p. 183-195 13 p. |
artikel |
28 |
Visualization of stagnation point inside the closed wake of a 20%-truncated plug nozzle at starting process
|
Mizukaki, Toshiharu |
|
2016 |
50 |
C |
p. 25-30 6 p. |
artikel |
29 |
Wake structure visualization of a flapping-wing Micro-Air-Vehicle in forward flight
|
Deng, Shuanghou |
|
2016 |
50 |
C |
p. 204-211 8 p. |
artikel |
30 |
Window based Multiple Model Adaptive Estimation for Navigational Framework
|
Kottath, Rahul |
|
2016 |
50 |
C |
p. 88-95 8 p. |
artikel |