A
-
Aeroacoustic simulation
Numerical calculation of the noise generated by air flow on different geometries [Volume 19, Issue 1, 2017, Pages 62-73]
-
Air-launched Systems
Analytical Model-based Fault Detection in Air-launched Systems Using Statistical Markov Models [Volume 19, Issue 2, 2017, Pages 29-43]
-
Airlines Companies
Evaluation the efficiency of Iran's airports by applying the two-stage Network of Data Envelopment Analysis method [Volume 19, Issue 2, 2017, Pages 12-28]
-
Airports
Evaluation the efficiency of Iran's airports by applying the two-stage Network of Data Envelopment Analysis method [Volume 19, Issue 2, 2017, Pages 12-28]
B
-
Blade Element Theory
Dynamic Modeling of Rotor Flapping Dynamics of an Unmanned Helicopter and Investigation of Applicability of System Identification and Control using Approximate Model [Volume 19, Issue 2, 2017, Pages 1-11]
C
-
Composite Cylinder
Damage detection and localization in a composite cylinder using FRF
curvature method [Volume 19, Issue 2, 2017, Pages 55-65]
D
-
Damage detection
Damage detection and localization in a composite cylinder using FRF
curvature method [Volume 19, Issue 2, 2017, Pages 55-65]
-
Data Envelopment Analysis
Evaluation the efficiency of Iran's airports by applying the two-stage Network of Data Envelopment Analysis method [Volume 19, Issue 2, 2017, Pages 12-28]
-
Delamination
Damage detection and localization in a composite cylinder using FRF
curvature method [Volume 19, Issue 2, 2017, Pages 55-65]
E
-
Efficiency
Evaluation the efficiency of Iran's airports by applying the two-stage Network of Data Envelopment Analysis method [Volume 19, Issue 2, 2017, Pages 12-28]
-
Energy harvesting
Reliability based design optimization of energy harvester from UAV engine vibration [Volume 19, Issue 1, 2017, Pages 50-61]
F
-
Ffowcs-Williams & Hawkings model
Numerical calculation of the noise generated by air flow on different geometries [Volume 19, Issue 1, 2017, Pages 62-73]
-
Flapping Dynamics
Dynamic Modeling of Rotor Flapping Dynamics of an Unmanned Helicopter and Investigation of Applicability of System Identification and Control using Approximate Model [Volume 19, Issue 2, 2017, Pages 1-11]
-
Fracture toughness
Experimental investigation of residual strength of aged aircrat structures [Volume 19, Issue 2, 2017, Pages 66-76]
-
FRF Curvature method
Damage detection and localization in a composite cylinder using FRF
curvature method [Volume 19, Issue 2, 2017, Pages 55-65]
K
-
Kalman Filter
Analytical Model-based Fault Detection in Air-launched Systems Using Statistical Markov Models [Volume 19, Issue 2, 2017, Pages 29-43]
L
-
Large Eddy Simulation
Numerical calculation of the noise generated by air flow on different geometries [Volume 19, Issue 1, 2017, Pages 62-73]
M
-
Main Rotor Modeling
Dynamic Modeling of Rotor Flapping Dynamics of an Unmanned Helicopter and Investigation of Applicability of System Identification and Control using Approximate Model [Volume 19, Issue 2, 2017, Pages 1-11]
-
Modal Analysis
Damage detection and localization in a composite cylinder using FRF
curvature method [Volume 19, Issue 2, 2017, Pages 55-65]
-
Model-based Fault Detection
Analytical Model-based Fault Detection in Air-launched Systems Using Statistical Markov Models [Volume 19, Issue 2, 2017, Pages 29-43]
P
-
Piezoelectric
Reliability based design optimization of energy harvester from UAV engine vibration [Volume 19, Issue 1, 2017, Pages 50-61]
-
Precipitation Hardening
Experimental investigation of residual strength of aged aircrat structures [Volume 19, Issue 2, 2017, Pages 66-76]
R
-
Reliability
Reliability based design optimization of energy harvester from UAV engine vibration [Volume 19, Issue 1, 2017, Pages 50-61]
S
-
Store separation
Numerical investigation of store separation from airplane wing, and study of the parameters, affecting the fall amount of store [Volume 19, Issue 2, 2017, Pages 44-54]
T
-
Two-Stage Network
Evaluation the efficiency of Iran's airports by applying the two-stage Network of Data Envelopment Analysis method [Volume 19, Issue 2, 2017, Pages 12-28]
U
-
UAV engine vibration
Reliability based design optimization of energy harvester from UAV engine vibration [Volume 19, Issue 1, 2017, Pages 50-61]
-
Unmanned Aerial Vehicle
Analytical Model-based Fault Detection in Air-launched Systems Using Statistical Markov Models [Volume 19, Issue 2, 2017, Pages 29-43]
-
Unmanned Rotorcraft
Dynamic Modeling of Rotor Flapping Dynamics of an Unmanned Helicopter and Investigation of Applicability of System Identification and Control using Approximate Model [Volume 19, Issue 2, 2017, Pages 1-11]
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