Journal of Aeronautical Engineering

Journal of Aeronautical Engineering

Keyword Index
A
  • Acoustic Analytical Model of Sound Transmission Through Infinite Laminated Composite Double Walled Cylindrical Shells [Volume 12, Issue 1, 2010, Pages 67-78]
  • Ad hoc On Design, Simulation, and Evaluation of a Secure Air Navigation Based on Multipath, Adaptive Loading and Wireless Ad Hoc Networks [Volume 12, Issue 2, 2010, Pages 23-32]
  • Anodizing Effect of Anodizing Conditions on Wear Resistance, Surface Hardness and Change of Dimensions on Aircraft Aluminum Alloys [Volume 12, Issue 2, 2010, Pages 45-54]
  • Aviation Accident Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
C
  • Canard Canard Geometry and Position Effects on the Wing Pressure Distribution of a Maneuverable Aircraft Model [Volume 12, Issue 1, 2010, Pages 11-31]
  • Canard Sweep Angle Canard Geometry and Position Effects on the Wing Pressure Distribution of a Maneuverable Aircraft Model [Volume 12, Issue 1, 2010, Pages 11-31]
  • Cartesian grid Generation of Cartesian Hybrid Grids for Aerodynamic Computation of Viscous Flows [Volume 12, Issue 2, 2010, Pages 1-11]
  • Coincidence frequency Analytical Model of Sound Transmission Through Infinite Laminated Composite Double Walled Cylindrical Shells [Volume 12, Issue 1, 2010, Pages 67-78]
  • Composite cylindrical sell Analytical Model of Sound Transmission Through Infinite Laminated Composite Double Walled Cylindrical Shells [Volume 12, Issue 1, 2010, Pages 67-78]
  • Composite materials Re-engineering of a Helicopter Structural Components Using Laminated Composite Materials Based on Crashworthiness Concepts [Volume 12, Issue 2, 2010, Pages 33-43]
  • Crashworthiness Re-engineering of a Helicopter Structural Components Using Laminated Composite Materials Based on Crashworthiness Concepts [Volume 12, Issue 2, 2010, Pages 33-43]
D
  • Downburst Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
  • Dynamic simulation Simulation of Milling Process in Roughening of Compressor Blade in Air Engine by Use of Finite Element Analysis [Volume 12, Issue 1, 2010, Pages 47-57]
E
  • EHD Air Flow Control at a Boundary Layer Using a Surface Dielectric Barrier Discharge Actuator [Volume 12, Issue 1, 2010, Pages 59-67]
F
  • F Factor Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
  • Finite Element Re-engineering of a Helicopter Structural Components Using Laminated Composite Materials Based on Crashworthiness Concepts [Volume 12, Issue 2, 2010, Pages 33-43]
  • Finite element method Simulation of Milling Process in Roughening of Compressor Blade in Air Engine by Use of Finite Element Analysis [Volume 12, Issue 1, 2010, Pages 47-57]
  • Flight Data Recorder Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
  • Flight simulation Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
H
  • Hardness Effect of Anodizing Conditions on Wear Resistance, Surface Hardness and Change of Dimensions on Aircraft Aluminum Alloys [Volume 12, Issue 2, 2010, Pages 45-54]
  • High speed milling Simulation of Milling Process in Roughening of Compressor Blade in Air Engine by Use of Finite Element Analysis [Volume 12, Issue 1, 2010, Pages 47-57]
  • Hysteresis Numerical Modeling of the Plate Behavior with Rotational Degree of Freedom and the Study of the Aerodynamic Hysteresis Phenomenon [Volume 12, Issue 2, 2010, Pages 13-22]
K
  • Knowledge Management Assessing the Readiness Degree of Organizations Working in Aerospace Industry for Transformation to Learning Organization [Volume 12, Issue 2, 2010, Pages 65-73]
L
  • Learning Assessing the Readiness Degree of Organizations Working in Aerospace Industry for Transformation to Learning Organization [Volume 12, Issue 2, 2010, Pages 65-73]
  • Learning Organization Assessing the Readiness Degree of Organizations Working in Aerospace Industry for Transformation to Learning Organization [Volume 12, Issue 2, 2010, Pages 65-73]
  • Linear Elastic Fracture Mechanics (LEFM) A Ritz and Harmonic Balance Solution Method for Dynamic Simulation of a Continuous Rotating System Containing an Active Crack [Volume 12, Issue 2, 2010, Pages 56-63]
  • Lower fuselage structure Re-engineering of a Helicopter Structural Components Using Laminated Composite Materials Based on Crashworthiness Concepts [Volume 12, Issue 2, 2010, Pages 33-43]
M
  • Mobile Ad Hoc Networks Design, Simulation, and Evaluation of a Secure Air Navigation Based on Multipath, Adaptive Loading and Wireless Ad Hoc Networks [Volume 12, Issue 2, 2010, Pages 23-32]
  • Multi Demand Distance Vector Design, Simulation, and Evaluation of a Secure Air Navigation Based on Multipath, Adaptive Loading and Wireless Ad Hoc Networks [Volume 12, Issue 2, 2010, Pages 23-32]
N
  • Navigation System network Design, Simulation, and Evaluation of a Secure Air Navigation Based on Multipath, Adaptive Loading and Wireless Ad Hoc Networks [Volume 12, Issue 2, 2010, Pages 23-32]
P
  • Pressure distribution Experimental Investigation of Pressure Distribution and Aerodynamic Coefficients in a Blade Cascade of an Airplane Engine Compressor [Volume 12, Issue 1, 2010, Pages 1-9]
  • Pressure distribution Canard Geometry and Position Effects on the Wing Pressure Distribution of a Maneuverable Aircraft Model [Volume 12, Issue 1, 2010, Pages 11-31]
R
  • Ring frequency Analytical Model of Sound Transmission Through Infinite Laminated Composite Double Walled Cylindrical Shells [Volume 12, Issue 1, 2010, Pages 67-78]
  • Ritz series A Ritz and Harmonic Balance Solution Method for Dynamic Simulation of a Continuous Rotating System Containing an Active Crack [Volume 12, Issue 2, 2010, Pages 56-63]
S
  • Security Design, Simulation, and Evaluation of a Secure Air Navigation Based on Multipath, Adaptive Loading and Wireless Ad Hoc Networks [Volume 12, Issue 2, 2010, Pages 23-32]
  • Stall phenomenon Experimental Investigation of Pressure Distribution and Aerodynamic Coefficients in a Blade Cascade of an Airplane Engine Compressor [Volume 12, Issue 1, 2010, Pages 1-9]
  • Strohaul number Numerical Modeling of the Plate Behavior with Rotational Degree of Freedom and the Study of the Aerodynamic Hysteresis Phenomenon [Volume 12, Issue 2, 2010, Pages 13-22]
T
  • Transmission Loss Analytical Model of Sound Transmission Through Infinite Laminated Composite Double Walled Cylindrical Shells [Volume 12, Issue 1, 2010, Pages 67-78]
V
  • Vortex Numerical Modeling of the Plate Behavior with Rotational Degree of Freedom and the Study of the Aerodynamic Hysteresis Phenomenon [Volume 12, Issue 2, 2010, Pages 13-22]
W
  • Wear-dimensions Effect of Anodizing Conditions on Wear Resistance, Surface Hardness and Change of Dimensions on Aircraft Aluminum Alloys [Volume 12, Issue 2, 2010, Pages 45-54]
  • Wind Estimation Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
  • Wind Tunnel Testing Canard Geometry and Position Effects on the Wing Pressure Distribution of a Maneuverable Aircraft Model [Volume 12, Issue 1, 2010, Pages 11-31]