Journal of Aeronautical Engineering

Journal of Aeronautical Engineering

Keyword Index
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]