A
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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]
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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]
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Aviation Accident
Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
C
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Canard
Canard Geometry and Position Effects on the Wing Pressure Distribution of a Maneuverable Aircraft Model [Volume 12, Issue 1, 2010, Pages 11-31]
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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]
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Cartesian grid
Generation of Cartesian Hybrid Grids for Aerodynamic Computation of Viscous Flows [Volume 12, Issue 2, 2010, Pages 1-11]
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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]
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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]
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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
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Downburst
Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
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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
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EHD
Air Flow Control at a Boundary Layer Using a Surface Dielectric Barrier Discharge Actuator [Volume 12, Issue 1, 2010, Pages 59-67]
F
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F Factor
Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
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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]
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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]
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Flight Data Recorder
Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
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Flight simulation
Investigation, Simulation & Analysis of Downburst-Related Aircraft Accidents Using FDR Data [Volume 12, Issue 1, 2010, Pages 33-46]
H
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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]
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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]
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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
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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
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Learning
Assessing the Readiness Degree of Organizations Working in Aerospace Industry for Transformation to Learning Organization [Volume 12, Issue 2, 2010, Pages 65-73]
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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]
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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]
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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
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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
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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]
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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
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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]
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