| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Accurate higher order automated unstructured triangular meshes for airfoil designs in aerospace applications using parabolic arcs
|
Supriya, Devi
|
|
2019
|
88 |
C |
p. 405-420
|
artikel
|
| 2 |
Adaptive fault tolerant control for a small coaxial rotor unmanned aerial vehicles with partial loss of actuator effectiveness
|
Song, Zhankui
|
|
2019
|
88 |
C |
p. 362-379
|
artikel
|
| 3 |
A droplet/wall impact model and simulation of a bipropellant rocket engine
|
Fu, Pengfei
|
|
2019
|
88 |
C |
p. 32-39
|
artikel
|
| 4 |
A method for optimizing the aerodynamic layout of a helicopter that reduces the effects of aerodynamic interaction
|
Lu, Yang
|
|
2019
|
88 |
C |
p. 73-83
|
artikel
|
| 5 |
An experimental study of the effects of different transverse trenches on depositing and temperature on a plate with film cooling holes
|
Liu, Zhengang
|
|
2019
|
88 |
C |
p. 40-50
|
artikel
|
| 6 |
Application of flow control strategy of blowing, synthetic and plasma jet actuators in vertical axis wind turbines
|
Zhu, Haitian
|
|
2019
|
88 |
C |
p. 468-480
|
artikel
|
| 7 |
A preliminary design procedure for an ion-beam shepherd mission
|
Urrutxua, Hodei
|
|
2019
|
88 |
C |
p. 421-435
|
artikel
|
| 8 |
Assessment of some stall-onset criteria for centrifugal compressors
|
Ghenaiet, Adel
|
|
2019
|
88 |
C |
p. 193-207
|
artikel
|
| 9 |
A Statistical Energy Analysis (SEA) model of a fuselage section for the prediction of the internal Sound Pressure Level (SPL) at cruise flight conditions
|
Petrone, Giuseppe
|
|
2019
|
88 |
C |
p. 340-349
|
artikel
|
| 10 |
Continuum breakdown and surface catalysis effects in NASA arc jet testing at SCIROCCO
|
Cinquegrana, Davide
|
|
2019
|
88 |
C |
p. 258-272
|
artikel
|
| 11 |
Control of cylinder wake flow and noise through a downstream porous treatment
|
Xu, Chen
|
|
2019
|
88 |
C |
p. 233-243
|
artikel
|
| 12 |
Cooperative guidance of seeker-less missile with two leaders
|
Zhao, Jianbo
|
|
2019
|
88 |
C |
p. 308-315
|
artikel
|
| 13 |
Design and aeromechanics investigation of compound helicopters
|
Yeo, Hyeonsoo
|
|
2019
|
88 |
C |
p. 158-173
|
artikel
|
| 14 |
4 Dimensional waypoint generation for conflict-free trajectory based operation
|
Sun, Minghui
|
|
2019
|
88 |
C |
p. 350-361
|
artikel
|
| 15 |
Editorial Board
|
|
|
2019
|
88 |
C |
p. ii
|
artikel
|
| 16 |
Effect of adverse pressure gradient on supersonic compressible boundary layer combustion
|
Zhang, Pu
|
|
2019
|
88 |
C |
p. 380-394
|
artikel
|
| 17 |
Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing
|
Sharifi Ghazijahani, Mohammad
|
|
2019
|
88 |
C |
p. 298-307
|
artikel
|
| 18 |
Electric sail trajectory design with Bezier curve-based shaping approach
|
Huo, Mingying
|
|
2019
|
88 |
C |
p. 126-135
|
artikel
|
| 19 |
Evaluation of the damping capacity according to the geometric and the number of resonator with thermal environment using a Rijke tube
|
Jo, Seonghwi
|
|
2019
|
88 |
C |
p. 1-8
|
artikel
|
| 20 |
Experimental investigation of the effect of extended cowl on the flow field of planar plug nozzles
|
Khan, Aqib
|
|
2019
|
88 |
C |
p. 208-221
|
artikel
|
| 21 |
Experimental investigation on delay time phenomenon in rotating detonation engine
|
Ma, John Z.
|
|
2019
|
88 |
C |
p. 395-404
|
artikel
|
| 22 |
Experimental investigation on the energy absorption characteristics of honeycomb sandwich panels under quasi-static punch loading
|
Zarei Mahmoudabadi, M.
|
|
2019
|
88 |
C |
p. 273-286
|
artikel
|
| 23 |
FV-MP model to predict lean blowout limits for multi-point lean direct injection combustors
|
Sun, Lei
|
|
2019
|
88 |
C |
p. 185-192
|
artikel
|
| 24 |
Geometrically nonlinear static aeroelastic analysis of composite morphing wing with corrugated structures
|
Tsushima, Natsuki
|
|
2019
|
88 |
C |
p. 244-257
|
artikel
|
| 25 |
High-dynamic baseline determination for the Swarm constellation
|
Mao, X.
|
|
2019
|
88 |
C |
p. 329-339
|
artikel
|
| 26 |
In-flight health monitoring of helicopter blades via differential analysis
|
Serafini, Jacopo
|
|
2019
|
88 |
C |
p. 436-443
|
artikel
|
| 27 |
Lateral cutoff analysis of sonic boom using full-field simulation
|
Yamashita, Rei
|
|
2019
|
88 |
C |
p. 316-328
|
artikel
|
| 28 |
Leakage and rotordynamic performance of T type labyrinth seal
|
Jia, Xingyun
|
|
2019
|
88 |
C |
p. 22-31
|
artikel
|
| 29 |
Numerical investigation of flame appearance and heat flux and in a deep-throttling variable thrust rocket engine
|
Jin, Yushu
|
|
2019
|
88 |
C |
p. 457-467
|
artikel
|
| 30 |
Optimal staging of serially staged rockets with velocity losses and fairing separation
|
Koch, Aaron D.
|
|
2019
|
88 |
C |
p. 65-72
|
artikel
|
| 31 |
Performance modeling of pulse detonation engines using the method of characteristics
|
Peace, James T.
|
|
2019
|
88 |
C |
p. 51-64
|
artikel
|
| 32 |
Rapid prototyping for hypervelocity impulse facility test models
|
Apirana, Steven F.T.
|
|
2019
|
88 |
C |
p. 174-184
|
artikel
|
| 33 |
Research of transition criterion for semi-empirical prediction method at specified transonic regime
|
Shi, Yayun
|
|
2019
|
88 |
C |
p. 95-109
|
artikel
|
| 34 |
Resonance avoidance for variable speed rotor blades using an applied compressive load
|
Dibble, Robert
|
|
2019
|
88 |
C |
p. 222-232
|
artikel
|
| 35 |
Rotorcraft blade-vortex interaction noise prediction using the Lattice-Boltzmann method
|
Romani, Gianluca
|
|
2019
|
88 |
C |
p. 147-157
|
artikel
|
| 36 |
Studies on the effect of imaging parameters on dynamic mode decomposition of time-resolved schlieren flow images
|
Rao, Srisha M.V.
|
|
2019
|
88 |
C |
p. 136-146
|
artikel
|
| 37 |
The impact of the length-to-depth ratio on aerodynamic surface quantities of a rarefied hypersonic cavity flow
|
Palharini, Rodrigo C.
|
|
2019
|
88 |
C |
p. 110-125
|
artikel
|
| 38 |
The optimization design with minimum power for variable speed control moment gyroscopes with integrated power and attitude control
|
Liu, Feng
|
|
2019
|
88 |
C |
p. 287-297
|
artikel
|
| 39 |
The potential of helicopter turboshaft engines incorporating highly effective recuperators under various flight conditions
|
Zhang, Chengyu
|
|
2019
|
88 |
C |
p. 84-94
|
artikel
|
| 40 |
Variable rotor speed and active blade twist for civil rotorcraft: Optimum scheduling, mission analysis, and environmental impact
|
Goulos, Ioannis
|
|
2019
|
88 |
C |
p. 444-456
|
artikel
|
| 41 |
Viscous flow and performance issues in a 6:1 supersonic mixed-flow compressor with a tandem diffuser
|
Sadagopan, Aravinth
|
|
2019
|
88 |
C |
p. 9-21
|
artikel
|
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