A
-
Active flow control
Numerical Simulation of several Structures of Plasma Actuators and Their Performance Assessment over NACA 0012 and NACA 0015 Airfoils [Volume 16, Issue 1, 2014, Pages 75-94]
-
Aerodynamics
Investigation of a Method for Aerodynamic and Inertial Loading on Aircraft Finite Element Model Using Genetic Algorithm and Mapping [Volume 16, Issue 1, 2014, Pages 65-74]
-
Airplane Systems
Classification of Advanced Training Jet Airplane by Using the Analytical Hierarchy Process (AHP) and Taxonomy Method [Volume 16, Issue 2, 2014, Pages 15-31]
-
Analytical hierarchy process (AHP)
Classification of Advanced Training Jet Airplane by Using the Analytical Hierarchy Process (AHP) and Taxonomy Method [Volume 16, Issue 2, 2014, Pages 15-31]
B
-
Backstepping
A Novel Robust Proportional Navigation Guidance Law for Surface-to-Air Missile Based on Extended Kalman Filter [Volume 16, Issue 1, 2014, Pages 33-48]
-
Bézier Curve
Continuous Curvature Trajectory Planning Based on Dubins Path and Bézier Curve for UAVs [Volume 16, Issue 1, 2014, Pages 49-64]
C
-
C-130 Hercules
Dynamic Modelling and Simulation of the Fuel Cell System for Supplying a Portion of Electric Energy of C-130 Hercules [Volume 16, Issue 1, 2014, Pages 1-16]
-
Calibration
Improvement of Accuracy by Pre-launch Compensation with Earth’s Gravity and Rotation Rate for SINS [Volume 16, Issue 1, 2014, Pages 95-104]
-
Continuous Curvature Trajectory
Continuous Curvature Trajectory Planning Based on Dubins Path and Bézier Curve for UAVs [Volume 16, Issue 1, 2014, Pages 49-64]
D
-
Dubins Path
Continuous Curvature Trajectory Planning Based on Dubins Path and Bézier Curve for UAVs [Volume 16, Issue 1, 2014, Pages 49-64]
E
-
Electro-Static Lumped-Element
Numerical Simulation of several Structures of Plasma Actuators and Their Performance Assessment over NACA 0012 and NACA 0015 Airfoils [Volume 16, Issue 1, 2014, Pages 75-94]
-
Error compensation
Improvement of Accuracy by Pre-launch Compensation with Earth’s Gravity and Rotation Rate for SINS [Volume 16, Issue 1, 2014, Pages 95-104]
F
-
Fiber-Metal Laminates
Effect of Impactor Energy and Layers Thickness on Fiber Metal Laminates in Low Velocity Impact [Volume 16, Issue 2, 2014, Pages 73-82]
-
Finite Element
Investigation of a Method for Aerodynamic and Inertial Loading on Aircraft Finite Element Model Using Genetic Algorithm and Mapping [Volume 16, Issue 1, 2014, Pages 65-74]
-
Flow Visualization
Experimental Investigation of Grid Winglet Effects on Aerodynamic Characteristics of a Wing Model at Low Reynolds Number [Volume 16, Issue 2, 2014, Pages 1-14]
-
Fuel Cell
Dynamic Modelling and Simulation of the Fuel Cell System for Supplying a Portion of Electric Energy of C-130 Hercules [Volume 16, Issue 1, 2014, Pages 1-16]
G
-
Genetic
A Novel Robust Proportional Navigation Guidance Law for Surface-to-Air Missile Based on Extended Kalman Filter [Volume 16, Issue 1, 2014, Pages 33-48]
-
Genetic Algorithm
Investigation of a Method for Aerodynamic and Inertial Loading on Aircraft Finite Element Model Using Genetic Algorithm and Mapping [Volume 16, Issue 1, 2014, Pages 65-74]
-
GRI
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
-
Grid Winglet
Experimental Investigation of Grid Winglet Effects on Aerodynamic Characteristics of a Wing Model at Low Reynolds Number [Volume 16, Issue 2, 2014, Pages 1-14]
-
Guided Projectile
Multidisciplinary and Multi-Objective Design Optimization of a Flying Projectile Using Evolutionary Algorithm (NSGA-II) [Volume 16, Issue 1, 2014, Pages 17-32]
-
Guide Vane
Experimental Investigation of the Effects of Variation in Guide Vanes Pitch and Curvature on Quality of Discharged Flow [Volume 16, Issue 2, 2014, Pages 83-93]
I
-
IFFT
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
-
Induced Drag Coefficient
Experimental Investigation of Grid Winglet Effects on Aerodynamic Characteristics of a Wing Model at Low Reynolds Number [Volume 16, Issue 2, 2014, Pages 1-14]
-
Inertial Navigation
Improvement of Accuracy by Pre-launch Compensation with Earth’s Gravity and Rotation Rate for SINS [Volume 16, Issue 1, 2014, Pages 95-104]
L
-
Lift Coefficient
Experimental Investigation of Grid Winglet Effects on Aerodynamic Characteristics of a Wing Model at Low Reynolds Number [Volume 16, Issue 2, 2014, Pages 1-14]
-
Loran System
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
-
Low Reynolds Number
Experimental Investigation of Grid Winglet Effects on Aerodynamic Characteristics of a Wing Model at Low Reynolds Number [Volume 16, Issue 2, 2014, Pages 1-14]
-
Low velocity impact
Effect of Impactor Energy and Layers Thickness on Fiber Metal Laminates in Low Velocity Impact [Volume 16, Issue 2, 2014, Pages 73-82]
M
-
Mapping
Investigation of a Method for Aerodynamic and Inertial Loading on Aircraft Finite Element Model Using Genetic Algorithm and Mapping [Volume 16, Issue 1, 2014, Pages 65-74]
-
Micro-turbine combustion chamber
Performance Analysis and Optimization of Micro-turbine Combustion Chamber by Numerical Simulation [Volume 16, Issue 2, 2014, Pages 47-62]
-
Monte Carlo simulation
Multidisciplinary and Multi-Objective Design Optimization of a Flying Projectile Using Evolutionary Algorithm (NSGA-II) [Volume 16, Issue 1, 2014, Pages 17-32]
-
Multidisciplinary design optimization
Multidisciplinary and Multi-Objective Design Optimization of a Flying Projectile Using Evolutionary Algorithm (NSGA-II) [Volume 16, Issue 1, 2014, Pages 17-32]
-
Multi-Objective Optimization
Multidisciplinary and Multi-Objective Design Optimization of a Flying Projectile Using Evolutionary Algorithm (NSGA-II) [Volume 16, Issue 1, 2014, Pages 17-32]
-
Music
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
N
-
NACA0012
Numerical Simulation of several Structures of Plasma Actuators and Their Performance Assessment over NACA 0012 and NACA 0015 Airfoils [Volume 16, Issue 1, 2014, Pages 75-94]
-
NACA0015
Numerical Simulation of several Structures of Plasma Actuators and Their Performance Assessment over NACA 0012 and NACA 0015 Airfoils [Volume 16, Issue 1, 2014, Pages 75-94]
-
Non-Dominated Sorting Genetic Algorithm II
Multidisciplinary and Multi-Objective Design Optimization of a Flying Projectile Using Evolutionary Algorithm (NSGA-II) [Volume 16, Issue 1, 2014, Pages 17-32]
P
-
Pilot training
Classification of Advanced Training Jet Airplane by Using the Analytical Hierarchy Process (AHP) and Taxonomy Method [Volume 16, Issue 2, 2014, Pages 15-31]
-
Pressure drop
Experimental Investigation of the Effects of Variation in Guide Vanes Pitch and Curvature on Quality of Discharged Flow [Volume 16, Issue 2, 2014, Pages 83-93]
-
Proportional navigation
A Novel Robust Proportional Navigation Guidance Law for Surface-to-Air Missile Based on Extended Kalman Filter [Volume 16, Issue 1, 2014, Pages 33-48]
R
-
Rayleigh’s criterion
Investigation of The Effect of Time Lag on Pressure Oscillations Amplitude Change in Premix Combustion [Volume 16, Issue 2, 2014, Pages 63-72]
S
-
Smooth Path Planning
Continuous Curvature Trajectory Planning Based on Dubins Path and Bézier Curve for UAVs [Volume 16, Issue 1, 2014, Pages 49-64]
-
Strapdown System
Improvement of Accuracy by Pre-launch Compensation with Earth’s Gravity and Rotation Rate for SINS [Volume 16, Issue 1, 2014, Pages 95-104]
T
-
Taxonomy
Classification of Advanced Training Jet Airplane by Using the Analytical Hierarchy Process (AHP) and Taxonomy Method [Volume 16, Issue 2, 2014, Pages 15-31]
-
Thermo acoustic instability
Investigation of The Effect of Time Lag on Pressure Oscillations Amplitude Change in Premix Combustion [Volume 16, Issue 2, 2014, Pages 63-72]
-
Time Differences of Arrival
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
-
Time of Arrival
Navigation Accuracy Improvement Using a New Integrated Algorithm of TOA/TDOA in Ground-based Loran Systems [Volume 16, Issue 2, 2014, Pages 33-46]
V
-
Velocity Distribution
Experimental Investigation of the Effects of Variation in Guide Vanes Pitch and Curvature on Quality of Discharged Flow [Volume 16, Issue 2, 2014, Pages 83-93]
W
-
Wind tunnel
Experimental Investigation of the Effects of Variation in Guide Vanes Pitch and Curvature on Quality of Discharged Flow [Volume 16, Issue 2, 2014, Pages 83-93]
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