| no |
title |
author |
magazine |
year |
volume |
issue |
page(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.
|
article
|
| 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.
|
article
|
| 3 |
Aircraft virtual sensor design via a Time-dependent Functional Pooling NARX methodology
|
Samara, Paraskevi A.
|
|
2013
|
29 |
1 |
p. 114-124
11 p.
|
article
|
| 4 |
A mode count procedure for mid-frequency analysis of complex vibro-acoustic systems
|
Roibás, E.
|
|
2013
|
29 |
1 |
p. 165-174
10 p.
|
article
|
| 5 |
Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft
|
Bernardini, G.
|
|
2013
|
29 |
1 |
p. 175-184
10 p.
|
article
|
| 6 |
Analysis of vibrations of an innovative civil tiltrotor
|
Gennaretti, M.
|
|
2013
|
29 |
1 |
p. 125-134
10 p.
|
article
|
| 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.
|
article
|
| 8 |
An efficient harmonic balance method for unsteady flows in cascades
|
Huang, Huang
|
|
2013
|
29 |
1 |
p. 144-154
11 p.
|
article
|
| 9 |
A new dynamic vector formed information sharing algorithm in federated filter
|
Xiong, Zhi
|
|
2013
|
29 |
1 |
p. 37-46
10 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 12 |
A study on simulation method of starlight transmission in hypersonic conditions
|
Yang, Bo
|
|
2013
|
29 |
1 |
p. 155-164
10 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 15 |
Design, performance evaluation and optimization of a UAV
|
Kontogiannis, Spyridon G.
|
|
2013
|
29 |
1 |
p. 339-350
12 p.
|
article
|
| 16 |
Development and implementation of an advanced, design-sensitive method for wing weight estimation
|
Elham, A.
|
|
2013
|
29 |
1 |
p. 100-113
14 p.
|
article
|
| 17 |
Dynamic analysis of damping mechanism in welded multilayered mild steel beams
|
Singh, Bhagat
|
|
2013
|
29 |
1 |
p. 58-73
16 p.
|
article
|
| 18 |
Dynamic bending response of thermoelastic functionally graded plates resting on elastic foundations
|
Zenkour, A.M.
|
|
2013
|
29 |
1 |
p. 7-17
11 p.
|
article
|
| 19 |
Editorial Board
|
|
|
2013
|
29 |
1 |
p. IFC-
1 p.
|
article
|
| 20 |
Effect of swirl on the regression rate in hybrid rocket motors
|
Kumar, C. Palani
|
|
2013
|
29 |
1 |
p. 92-99
8 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 24 |
ISHM-based intelligent fusion prognostics for space avionics
|
Ding, Can
|
|
2013
|
29 |
1 |
p. 200-205
6 p.
|
article
|
| 25 |
Lagwise dynamic analysis of a variable speed rotor
|
Han, Dong
|
|
2013
|
29 |
1 |
p. 277-286
10 p.
|
article
|
| 26 |
Loosely coupled multibody dynamics–CFD analysis for a rotor in descending flight
|
Park, Jae-Sang
|
|
2013
|
29 |
1 |
p. 262-276
15 p.
|
article
|
| 27 |
Modeling and control of a helicopter slung-load system
|
Oktay, Tugrul
|
|
2013
|
29 |
1 |
p. 206-222
17 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 33 |
Optimization of astronaut landing position based on micro multi-objective genetic algorithms
|
Liu, Xin
|
|
2013
|
29 |
1 |
p. 321-329
9 p.
|
article
|
| 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.
|
article
|
| 35 |
Passive vibration control of flexible spacecraft using shunted piezoelectric transducers
|
Sales, T.P.
|
|
2013
|
29 |
1 |
p. 403-412
10 p.
|
article
|
| 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.
|
article
|
| 37 |
Receptacle normal position control for automated aerial refueling
|
Kriel, S.C.
|
|
2013
|
29 |
1 |
p. 296-304
9 p.
|
article
|
| 38 |
Research on inflight parameter identification and icing location detection of the aircraft
|
Dong, Yiqun
|
|
2013
|
29 |
1 |
p. 305-312
8 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 41 |
Thermal control of spaceborne image sensor using heat pipe cooling system
|
Oh, Hyun-Ung
|
|
2013
|
29 |
1 |
p. 394-402
9 p.
|
article
|
| 42 |
Thermally induced vibrations of flexible beams using Absolute Nodal Coordinate Formulation
|
Shen, Zhenxing
|
|
2013
|
29 |
1 |
p. 386-393
8 p.
|
article
|
| 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.
|
article
|
| 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.
|
article
|
| 45 |
Variable transpiration cooling for the thermal management of reusable hypersonic vehicles
|
Gulli, S.
|
|
2013
|
29 |
1 |
p. 434-444
11 p.
|
article
|
| 46 |
Vortex formation on squared and rounded tip
|
Giuni, Michea
|
|
2013
|
29 |
1 |
p. 191-199
9 p.
|
article
|
Journal description