| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
A comparison of time and frequency domain descriptions of high frequency acoustics in rocket engines with focus on dome coupling
|
Schulze, M.
|
|
2015
|
45 |
C |
p. 165-173
9 p.
|
artikel
|
| 2 |
Actuator placement robust optimization for vibration control system with interval parameters
|
Li, Yunlong
|
|
2015
|
45 |
C |
p. 88-98
11 p.
|
artikel
|
| 3 |
Analysis of jet blast impact of embarked aircraft on deck takeoff zone
|
Yue, Kuizhi
|
|
2015
|
45 |
C |
p. 60-66
7 p.
|
artikel
|
| 4 |
Analysis of transitional flow in 3D geometries using a novel phenomenological model
|
Vizinho, Rui
|
|
2015
|
45 |
C |
p. 431-441
11 p.
|
artikel
|
| 5 |
Analytical solution for the free vibration characteristics of the rotating composite beams with a delamination
|
Jafari-Talookolaei, Ramazan-Ali
|
|
2015
|
45 |
C |
p. 346-358
13 p.
|
artikel
|
| 6 |
A new GPS-based calibration of GRACE accelerometers using the arc-to-chord threshold uncovered sinusoidal disturbing signal
|
Calabia, Andrés
|
|
2015
|
45 |
C |
p. 265-271
7 p.
|
artikel
|
| 7 |
An indirect adaptive predictive control for the pitch channel autopilot of a flight system
|
Salahshoor, Karim
|
|
2015
|
45 |
C |
p. 78-87
10 p.
|
artikel
|
| 8 |
An investigation of on-orbit release with inter-satellite electromagnetic force
|
Zhang, Yuan-wen
|
|
2015
|
45 |
C |
p. 309-315
7 p.
|
artikel
|
| 9 |
A novel nonlinear hybrid controller design for an uncertain quadrotor with disturbances
|
Modirrousta, Alireza
|
|
2015
|
45 |
C |
p. 294-308
15 p.
|
artikel
|
| 10 |
A numerical investigation of oxidizer mixed hybrid rocket motors
|
Chidambaram, Palani Kumar
|
|
2015
|
45 |
C |
p. 10-16
7 p.
|
artikel
|
| 11 |
A station-keeping control method for GEO spacecraft based on autonomous control architecture
|
Yang, Wenbo
|
|
2015
|
45 |
C |
p. 462-475
14 p.
|
artikel
|
| 12 |
A structured H ∞ -based optimization approach for integrated plant and self-scheduled flight control system design
|
Lhachemi, H.
|
|
2015
|
45 |
C |
p. 30-38
9 p.
|
artikel
|
| 13 |
Blended secondary surveillance radar solutions to improve air traffic surveillance
|
Kim, Euiho
|
|
2015
|
45 |
C |
p. 203-208
6 p.
|
artikel
|
| 14 |
Cassiopee: A CFD pre- and post-processing tool
|
Benoit, Christophe
|
|
2015
|
45 |
C |
p. 272-283
12 p.
|
artikel
|
| 15 |
Conceptual redesign of the B-1B bomber inlets for improved supersonic performance
|
Berra, Lee M.
|
|
2015
|
45 |
C |
p. 476-483
8 p.
|
artikel
|
| 16 |
Control of base pressure for a boat-tailed axisymmetric afterbody via base geometry modifications
|
Tripathi, Akriti
|
|
2015
|
45 |
C |
p. 284-293
10 p.
|
artikel
|
| 17 |
Determination and verification of Johnson–Cook model parameters at high-speed deformation of titanium alloys
|
Buzyurkin, A.E.
|
|
2015
|
45 |
C |
p. 121-127
7 p.
|
artikel
|
| 18 |
4D trajectory estimation based on nominal flight profile extraction and airway meteorological forecast revision
|
Tang, Xinmin
|
|
2015
|
45 |
C |
p. 387-397
11 p.
|
artikel
|
| 19 |
Editorial Board
|
|
|
2015
|
45 |
C |
p. IFC-
1 p.
|
artikel
|
| 20 |
Effect of elastic deformation on the aerodynamic characteristics of a high-speed spinning projectile
|
Yin, Jintao
|
|
2015
|
45 |
C |
p. 254-264
11 p.
|
artikel
|
| 21 |
Effect of elastic deformation on the trajectory of aerial separation
|
Hua, RuHao
|
|
2015
|
45 |
C |
p. 128-139
12 p.
|
artikel
|
| 22 |
Effect of fiber tension on the deformation of a carbon composite plate for space radio telescopes
|
Bitkina, Olga
|
|
2015
|
45 |
C |
p. 99-103
5 p.
|
artikel
|
| 23 |
Effects of aerodynamic modeling on the optimal wing kinematics for hovering MAVs
|
Yan, Zhimiao
|
|
2015
|
45 |
C |
p. 39-49
11 p.
|
artikel
|
| 24 |
Engine pre-entry thrust and standard net thrust evaluation based on the far-field method
|
Malouin, Benoit
|
|
2015
|
45 |
C |
p. 50-59
10 p.
|
artikel
|
| 25 |
Experimental characterization of water droplet deformation and breakup in the vicinity of a moving airfoil
|
García-Magariño, A.
|
|
2015
|
45 |
C |
p. 490-500
11 p.
|
artikel
|
| 26 |
Experimental study on on-orbit and launch environment vibration isolation performance of a vibration isolator using bellows and viscous fluid
|
Lee, Dae-Oen
|
|
2015
|
45 |
C |
p. 1-9
9 p.
|
artikel
|
| 27 |
Experimental testing of mini heat pipes under microgravity conditions aboard a suborbital rocket
|
Paiva, K.V.
|
|
2015
|
45 |
C |
p. 367-375
9 p.
|
artikel
|
| 28 |
Finite element model updating of a space vehicle first stage motor based on experimental test results
|
Raja Mohamed Rabi, B.
|
|
2015
|
45 |
C |
p. 422-430
9 p.
|
artikel
|
| 29 |
Flying by the Sun only: The Solarcopter prototype
|
Shaheed, M. Hasan
|
|
2015
|
45 |
C |
p. 209-214
6 p.
|
artikel
|
| 30 |
Fully coupled thermo-mechanical analysis of bi-directional FGM beams using NURBS isogeometric finite element approach
|
Lezgy-Nazargah, M.
|
|
2015
|
45 |
C |
p. 154-164
11 p.
|
artikel
|
| 31 |
High altitude propeller design and analysis
|
Morgado, J.
|
|
2015
|
45 |
C |
p. 398-407
10 p.
|
artikel
|
| 32 |
High angle of attack command generation technique and tracking control for agile missiles
|
Ma, Yueyue
|
|
2015
|
45 |
C |
p. 324-334
11 p.
|
artikel
|
| 33 |
Identification of nonlinear characteristics of pressure fluctuations at spontaneous combustion instabilities
|
Seo, Seonghyeon
|
|
2015
|
45 |
C |
p. 114-120
7 p.
|
artikel
|
| 34 |
Interplanetary trajectory design for a hybrid propulsion system
|
Gong, Shengping
|
|
2015
|
45 |
C |
p. 104-113
10 p.
|
artikel
|
| 35 |
Investigation of the influence of co-flow velocity ratio on a compressible plane jet exhausting into parallel streams
|
Datta, Abanti
|
|
2015
|
45 |
C |
p. 186-195
10 p.
|
artikel
|
| 36 |
Kinematically coupled spacecraft relative motion without attitude synchronization assumption
|
Lee, Daero
|
|
2015
|
45 |
C |
p. 316-323
8 p.
|
artikel
|
| 37 |
Mars atmospheric entry guidance for reference trajectory tracking
|
Dai, Juan
|
|
2015
|
45 |
C |
p. 335-345
11 p.
|
artikel
|
| 38 |
Maximum allowable load of very flexible manipulators by using absolute nodal coordinate
|
Heidari, H.R.
|
|
2015
|
45 |
C |
p. 67-77
11 p.
|
artikel
|
| 39 |
Maximum endurance for battery-powered rotary-wing aircraft
|
Gatti, Mauro
|
|
2015
|
45 |
C |
p. 174-179
6 p.
|
artikel
|
| 40 |
Microstructure and superplastic deformation for aerospace Ti-alloys associated with α-phase curing behavior
|
Ning, Y.Q.
|
|
2015
|
45 |
C |
p. 416-421
6 p.
|
artikel
|
| 41 |
Multi-fidelity robust aerodynamic design optimization under mixed uncertainty
|
Shah, Harsheel
|
|
2015
|
45 |
C |
p. 17-29
13 p.
|
artikel
|
| 42 |
Nonlinear control of an air-breathing engine including its validation with vehicle guidance
|
Maity, Arnab
|
|
2015
|
45 |
C |
p. 242-253
12 p.
|
artikel
|
| 43 |
Numerical study of three dimensional acoustic resonances in open cavities at high Reynolds numbers
|
Kompenhans, M.
|
|
2015
|
45 |
C |
p. 501-511
11 p.
|
artikel
|
| 44 |
Optimal nonlinear feedback guidance algorithm for Mars powered descent
|
Zheng, Yiyu
|
|
2015
|
45 |
C |
p. 359-366
8 p.
|
artikel
|
| 45 |
Optimization control for the far-distance rapid cooperative rendezvous of spacecraft with different masses
|
Feng, Weiming
|
|
2015
|
45 |
C |
p. 449-461
13 p.
|
artikel
|
| 46 |
Performance of a ducted propeller designed for UAV applications at zero angle of attack flight: An experimental study
|
Yilmaz, S.
|
|
2015
|
45 |
C |
p. 376-386
11 p.
|
artikel
|
| 47 |
Results of the pilot assistance system “Assisted Low-Level Flight and Landing on Unprepared Landing Sites” obtained with the ACT/FHS research rotorcraft
|
Greiser, Steffen
|
|
2015
|
45 |
C |
p. 215-227
13 p.
|
artikel
|
| 48 |
Robust adaptive control for attitude tracking of spacecraft with unknown dead-zone
|
Wu, Baolin
|
|
2015
|
45 |
C |
p. 196-202
7 p.
|
artikel
|
| 49 |
Robust trim procedure for rotorcraft configurations
|
Friedman, Chen
|
|
2015
|
45 |
C |
p. 442-448
7 p.
|
artikel
|
| 50 |
Spar disbond visualization in in-service composite UAV with ultrasonic propagation imager
|
Lee, Jung-Ryul
|
|
2015
|
45 |
C |
p. 180-185
6 p.
|
artikel
|
| 51 |
Switching control of thrust regulation and inlet unstart protection for scramjet engine based on strategy of integral initial values resetting
|
Cao, Ruifeng
|
|
2015
|
45 |
C |
p. 484-489
6 p.
|
artikel
|
| 52 |
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion
|
Yao, Zhaopu
|
|
2015
|
45 |
C |
p. 140-149
10 p.
|
artikel
|
| 53 |
Universal erosive burning model performance for solid rocket motor internal ballistics
|
Javed, Afroz
|
|
2015
|
45 |
C |
p. 150-153
4 p.
|
artikel
|
| 54 |
Vibration reduction in aerospace structures via an optimized modified positive velocity feedback control
|
Omidi, Ehsan
|
|
2015
|
45 |
C |
p. 408-415
8 p.
|
artikel
|
| 55 |
Zero Poisson's ratio flexible skin for potential two-dimensional wing morphing
|
Chen, Jinjin
|
|
2015
|
45 |
C |
p. 228-241
14 p.
|
artikel
|
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