nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
1 |
A data processing method in the experiment of heat flux testing using inverse methods
|
Shi, You-An |
|
2013 |
29 |
1 |
p. 74-80 7 p. |
artikel |
2 |
Aerodynamic analysis and optimization of a transonic axial compressor with casing grooves to improve operating stability
|
Kim, Jin-Hyuk |
|
2013 |
29 |
1 |
p. 81-91 11 p. |
artikel |
3 |
Aircraft virtual sensor design via a Time-dependent Functional Pooling NARX methodology
|
Samara, Paraskevi A. |
|
2013 |
29 |
1 |
p. 114-124 11 p. |
artikel |
4 |
A mode count procedure for mid-frequency analysis of complex vibro-acoustic systems
|
Roibás, E. |
|
2013 |
29 |
1 |
p. 165-174 10 p. |
artikel |
5 |
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft
|
Bernardini, G. |
|
2013 |
29 |
1 |
p. 175-184 10 p. |
artikel |
6 |
Analysis of vibrations of an innovative civil tiltrotor
|
Gennaretti, M. |
|
2013 |
29 |
1 |
p. 125-134 10 p. |
artikel |
7 |
Analytical modeling to predict the low velocity impact response of circular GLARE fiber–metal laminates
|
Tsamasphyros, George J. |
|
2013 |
29 |
1 |
p. 28-36 9 p. |
artikel |
8 |
An efficient harmonic balance method for unsteady flows in cascades
|
Huang, Huang |
|
2013 |
29 |
1 |
p. 144-154 11 p. |
artikel |
9 |
A new dynamic vector formed information sharing algorithm in federated filter
|
Xiong, Zhi |
|
2013 |
29 |
1 |
p. 37-46 10 p. |
artikel |
10 |
A novel adaptive importance sampling algorithm based on Markov chain and low-discrepancy sequence
|
Yuan, Xiukai |
|
2013 |
29 |
1 |
p. 253-261 9 p. |
artikel |
11 |
A study on forced vibration behaviors of composite main wing structure of the 20 seat class small scale WIG craft
|
Park, Hyunbum |
|
2013 |
29 |
1 |
p. 445-452 8 p. |
artikel |
12 |
A study on simulation method of starlight transmission in hypersonic conditions
|
Yang, Bo |
|
2013 |
29 |
1 |
p. 155-164 10 p. |
artikel |
13 |
Control allocation performance for blended wing body aircraft and its impact on control surface design
|
Waters, Stephen M. |
|
2013 |
29 |
1 |
p. 18-27 10 p. |
artikel |
14 |
Designing anti-swing fuzzy controller for helicopter slung-load system near hover by particle swarms
|
Omar, Hanafy M. |
|
2013 |
29 |
1 |
p. 223-234 12 p. |
artikel |
15 |
Design, performance evaluation and optimization of a UAV
|
Kontogiannis, Spyridon G. |
|
2013 |
29 |
1 |
p. 339-350 12 p. |
artikel |
16 |
Development and implementation of an advanced, design-sensitive method for wing weight estimation
|
Elham, A. |
|
2013 |
29 |
1 |
p. 100-113 14 p. |
artikel |
17 |
Dynamic analysis of damping mechanism in welded multilayered mild steel beams
|
Singh, Bhagat |
|
2013 |
29 |
1 |
p. 58-73 16 p. |
artikel |
18 |
Dynamic bending response of thermoelastic functionally graded plates resting on elastic foundations
|
Zenkour, A.M. |
|
2013 |
29 |
1 |
p. 7-17 11 p. |
artikel |
19 |
Editorial Board
|
|
|
2013 |
29 |
1 |
p. IFC- 1 p. |
artikel |
20 |
Effect of swirl on the regression rate in hybrid rocket motors
|
Kumar, C. Palani |
|
2013 |
29 |
1 |
p. 92-99 8 p. |
artikel |
21 |
Experimental and numerical comparison of cold expansion and interference fit methods in improving fatigue life of holed plate in double shear lap joints
|
Chakherlou, T.N. |
|
2013 |
29 |
1 |
p. 351-362 12 p. |
artikel |
22 |
Experimental study on barely visible impact damage and visible impact damage for repair of small aircraft composite structure
|
Park, Hyunbum |
|
2013 |
29 |
1 |
p. 363-372 10 p. |
artikel |
23 |
Impact of the fuselage damping characteristics and the blade rigidity on the stability of helicopter
|
Chellil, A. |
|
2013 |
29 |
1 |
p. 235-252 18 p. |
artikel |
24 |
ISHM-based intelligent fusion prognostics for space avionics
|
Ding, Can |
|
2013 |
29 |
1 |
p. 200-205 6 p. |
artikel |
25 |
Lagwise dynamic analysis of a variable speed rotor
|
Han, Dong |
|
2013 |
29 |
1 |
p. 277-286 10 p. |
artikel |
26 |
Loosely coupled multibody dynamics–CFD analysis for a rotor in descending flight
|
Park, Jae-Sang |
|
2013 |
29 |
1 |
p. 262-276 15 p. |
artikel |
27 |
Modeling and control of a helicopter slung-load system
|
Oktay, Tugrul |
|
2013 |
29 |
1 |
p. 206-222 17 p. |
artikel |
28 |
Modelling and configuration control of wing-shaped bi-stable piezoelectric composites under aerodynamic loads
|
Arrieta, Andres F. |
|
2013 |
29 |
1 |
p. 453-461 9 p. |
artikel |
29 |
Modification of the critical projectile diameter of honeycomb sandwich panel considering the channeling effect in hypervelocity impact
|
Kang, Pilseong |
|
2013 |
29 |
1 |
p. 413-425 13 p. |
artikel |
30 |
Multifunctional fuel cell system in an aircraft environment: An investigation focusing on fuel tank inerting and water generation
|
Keim, Martin |
|
2013 |
29 |
1 |
p. 330-338 9 p. |
artikel |
31 |
Nonlinear finite element analysis of thermal post-buckling vibration of laminated composite shell panel embedded with SMA fibre
|
Panda, Subrata Kumar |
|
2013 |
29 |
1 |
p. 47-57 11 p. |
artikel |
32 |
On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding
|
Gennaro, Elmer M. |
|
2013 |
29 |
1 |
p. 313-320 8 p. |
artikel |
33 |
Optimization of astronaut landing position based on micro multi-objective genetic algorithms
|
Liu, Xin |
|
2013 |
29 |
1 |
p. 321-329 9 p. |
artikel |
34 |
Output feedback control for free-floating space robotic manipulators base on adaptive fuzzy neural network
|
Zhang, WenHui |
|
2013 |
29 |
1 |
p. 135-143 9 p. |
artikel |
35 |
Passive vibration control of flexible spacecraft using shunted piezoelectric transducers
|
Sales, T.P. |
|
2013 |
29 |
1 |
p. 403-412 10 p. |
artikel |
36 |
Performance investigation of variable damping shock absorber combined with conventional semi-active vibration control logics
|
Oh, Hyun-Ung |
|
2013 |
29 |
1 |
p. 1-6 6 p. |
artikel |
37 |
Receptacle normal position control for automated aerial refueling
|
Kriel, S.C. |
|
2013 |
29 |
1 |
p. 296-304 9 p. |
artikel |
38 |
Research on inflight parameter identification and icing location detection of the aircraft
|
Dong, Yiqun |
|
2013 |
29 |
1 |
p. 305-312 8 p. |
artikel |
39 |
Short-term consequences of radio communications blackout on the U.S. National Airspace System
|
Palacios, Rafael |
|
2013 |
29 |
1 |
p. 426-433 8 p. |
artikel |
40 |
Some compressibility effects on the lee side flow structures of cruciform wing–body configurations with very low aspect ratio wings
|
Tuling, S. |
|
2013 |
29 |
1 |
p. 373-385 13 p. |
artikel |
41 |
Thermal control of spaceborne image sensor using heat pipe cooling system
|
Oh, Hyun-Ung |
|
2013 |
29 |
1 |
p. 394-402 9 p. |
artikel |
42 |
Thermally induced vibrations of flexible beams using Absolute Nodal Coordinate Formulation
|
Shen, Zhenxing |
|
2013 |
29 |
1 |
p. 386-393 8 p. |
artikel |
43 |
Towards the use of mushroom-capped dry adhesives in outer space: Effects of low pressure and temperature on adhesion strength
|
Henrey, Michael |
|
2013 |
29 |
1 |
p. 185-190 6 p. |
artikel |
44 |
Using an effective tabu search in interactive resources scheduling problem for LEO satellites missions
|
Sarkheyli, Arezoo |
|
2013 |
29 |
1 |
p. 287-295 9 p. |
artikel |
45 |
Variable transpiration cooling for the thermal management of reusable hypersonic vehicles
|
Gulli, S. |
|
2013 |
29 |
1 |
p. 434-444 11 p. |
artikel |
46 |
Vortex formation on squared and rounded tip
|
Giuni, Michea |
|
2013 |
29 |
1 |
p. 191-199 9 p. |
artikel |