| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A Boolean algebraic-based solution for multiple fault diagnosis: Application to a spatial mission
|
Issury, Irwin
|
|
2013
|
28 |
1 |
p. 214-226
13 p.
|
artikel
|
| 2 |
Aerodynamic shape optimization of hovering rotor blades using a coupled free wake–CFD and adjoint method
|
Farrokhfal, H.
|
|
2013
|
28 |
1 |
p. 21-30
10 p.
|
artikel
|
| 3 |
Aerodynamic technologies to improve aircraft performance
|
Abbas, A.
|
|
2013
|
28 |
1 |
p. 100-132
33 p.
|
artikel
|
| 4 |
Aircraft tracking by means of the Acoustical Doppler Effect
|
Martín, Sara R.
|
|
2013
|
28 |
1 |
p. 305-314
10 p.
|
artikel
|
| 5 |
Analysis of Pareto frontiers for multidisciplinary design optimization of aircraft
|
Mastroddi, Franco
|
|
2013
|
28 |
1 |
p. 40-55
16 p.
|
artikel
|
| 6 |
An analytical approach for stand-off distance of detached shock waves
|
Askari, S.
|
|
2013
|
28 |
1 |
p. 384-390
7 p.
|
artikel
|
| 7 |
A new bird model and the effect of bird geometry in impacts from various orientations
|
Hedayati, Reza
|
|
2013
|
28 |
1 |
p. 9-20
12 p.
|
artikel
|
| 8 |
An investigation on vertical tailplane contribution to aircraft sideforce
|
Nicolosi, Fabrizio
|
|
2013
|
28 |
1 |
p. 401-416
16 p.
|
artikel
|
| 9 |
A passive launch and on-orbit vibration isolation system for the spaceborne cryocooler
|
Oh, Hyun-Ung
|
|
2013
|
28 |
1 |
p. 324-331
8 p.
|
artikel
|
| 10 |
A sliding mode controller for aircraft simulated entry into spin
|
Venkateswara Rao, D.M.K.K.
|
|
2013
|
28 |
1 |
p. 154-163
10 p.
|
artikel
|
| 11 |
A Weighted Measurement Fusion Kalman Filter implementation for UAV navigation
|
Goh, Shu Ting
|
|
2013
|
28 |
1 |
p. 315-323
9 p.
|
artikel
|
| 12 |
Challenges in the aerodynamics modeling of an oscillating and translating airfoil at large incidence angles
|
Ghoreyshi, Mehdi
|
|
2013
|
28 |
1 |
p. 176-190
15 p.
|
artikel
|
| 13 |
Comments on the paper “Chaotic motions of a two-dimensional airfoil with cubic nonlinearity in supersonic flow”
|
Algaba, Antonio
|
|
2013
|
28 |
1 |
p. 431-434
4 p.
|
artikel
|
| 14 |
Comparative studies on flow control in rectangular S-duct diffuser using submerged-vortex generators
|
Paul, Akshoy Ranjan
|
|
2013
|
28 |
1 |
p. 332-343
12 p.
|
artikel
|
| 15 |
Computational approximation of nonlinear unsteady aerodynamics using an aerodynamic model hierarchy
|
Ghoreyshi, Mehdi
|
|
2013
|
28 |
1 |
p. 133-144
12 p.
|
artikel
|
| 16 |
Control allocation for an over-actuated Satellite Launch Vehicle
|
Kishore, W.C. Arun
|
|
2013
|
28 |
1 |
p. 56-71
16 p.
|
artikel
|
| 17 |
Editorial Board
|
|
|
2013
|
28 |
1 |
p. IFC-
1 p.
|
artikel
|
| 18 |
Effect of non-uniform mean flow field on acoustic propagation problems in computational aeroacoustics
|
Si, Haiqing
|
|
2013
|
28 |
1 |
p. 145-153
9 p.
|
artikel
|
| 19 |
Evaluation of radiative heat transfer for interplanetary re-entry under vibrational nonequilibrium conditions
|
Mazzoni, C.M.
|
|
2013
|
28 |
1 |
p. 191-197
7 p.
|
artikel
|
| 20 |
FIA method for LBO limit predictions of aero-engine combustors based on FV model
|
Hu, Bin
|
|
2013
|
28 |
1 |
p. 435-446
12 p.
|
artikel
|
| 21 |
Hypersonic vehicle thermal protection system model optimization and validation with vibration tests
|
Tobe, Randy J.
|
|
2013
|
28 |
1 |
p. 208-213
6 p.
|
artikel
|
| 22 |
Improvement of structures vibroacoustics by widespread embodiment of viscoelastic materials
|
Ghiringhelli, G.L.
|
|
2013
|
28 |
1 |
p. 227-241
15 p.
|
artikel
|
| 23 |
INS/VisNav/GPS relative navigation system for UAV
|
Wang, Xiaogang
|
|
2013
|
28 |
1 |
p. 242-248
7 p.
|
artikel
|
| 24 |
Inverse optimal and robust nonlinear attitude control of rigid spacecraft
|
Park, Yonmook
|
|
2013
|
28 |
1 |
p. 257-265
9 p.
|
artikel
|
| 25 |
Investigation of drag and wake turbulence of a rotor hub
|
Raghav, Vrishank
|
|
2013
|
28 |
1 |
p. 164-175
12 p.
|
artikel
|
| 26 |
Latin hypercube sampling applied to reliability-based multidisciplinary design optimization of a launch vehicle
|
Roshanian, Jafar
|
|
2013
|
28 |
1 |
p. 297-304
8 p.
|
artikel
|
| 27 |
Linear stability analysis of a slightly viscoelastic liquid jet
|
Yang, Li-jun
|
|
2013
|
28 |
1 |
p. 249-256
8 p.
|
artikel
|
| 28 |
Mixed-mode crack propagation of stiffened curved panels repaired by composite patch under combined tension and shear cyclic loading
|
Hosseini-Toudeshky, Hossein
|
|
2013
|
28 |
1 |
p. 344-363
20 p.
|
artikel
|
| 29 |
Numerical and experimental investigation of infrared radiation characteristics of a turbofan engine exhaust system with film cooling central body
|
Shan, Yong
|
|
2013
|
28 |
1 |
p. 281-288
8 p.
|
artikel
|
| 30 |
Numerical prediction on the interaction between the incident shock wave and the transverse slot injection in supersonic flows
|
Huang, Wei
|
|
2013
|
28 |
1 |
p. 91-99
9 p.
|
artikel
|
| 31 |
On the damping of ultrasonic transducersʼ components
|
Abdullah, Amir
|
|
2013
|
28 |
1 |
p. 31-39
9 p.
|
artikel
|
| 32 |
Optimising the locations of thermally sensitive equipment in an aircraft crown compartment
|
Butler, C.
|
|
2013
|
28 |
1 |
p. 391-400
10 p.
|
artikel
|
| 33 |
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
|
Li, Fei
|
|
2013
|
28 |
1 |
p. 72-78
7 p.
|
artikel
|
| 34 |
Propulsive characteristics of metal fuel-rich pyrotechnics in hydro-reactive motors
|
Ghassemi, Hojat
|
|
2013
|
28 |
1 |
p. 1-8
8 p.
|
artikel
|
| 35 |
Quasi-continuous high-order sliding mode controller design for reusable launch vehicles in reentry phase
|
Tian, Bailing
|
|
2013
|
28 |
1 |
p. 198-207
10 p.
|
artikel
|
| 36 |
Robust Adaptive Kalman Filter for estimation of UAV dynamics in the presence of sensor/actuator faults
|
Hajiyev, Chingiz
|
|
2013
|
28 |
1 |
p. 376-383
8 p.
|
artikel
|
| 37 |
Spacecraft attitude tracking control under actuator magnitude deviation and misalignment
|
Hu, Qinglei
|
|
2013
|
28 |
1 |
p. 266-280
15 p.
|
artikel
|
| 38 |
Sun–Earth–Moon autonomous orbit determination for quasi-periodic orbit about the translunar libration point and its observability analysis
|
Qian, Yingjing
|
|
2013
|
28 |
1 |
p. 289-296
8 p.
|
artikel
|
| 39 |
The effect of angle of attack on the flow structure over the nonslender lambda wing
|
Yayla, S.
|
|
2013
|
28 |
1 |
p. 417-430
14 p.
|
artikel
|
| 40 |
The Zigzag wingbox for a span morphing wing
|
Ajaj, R.M.
|
|
2013
|
28 |
1 |
p. 364-375
12 p.
|
artikel
|
| 41 |
Unsteady fluid–structure interactions of a pitching membrane wing
|
Tregidgo, L.
|
|
2013
|
28 |
1 |
p. 79-90
12 p.
|
artikel
|
Tijdschrift beschrijving