Keyword Index

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]