Keyword Index

A

  • Airfoil Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015 [Volume 8, Issue 1, 2011, Pages 1-10]
  • Axiomatic Design A Novel Approach to Design of Truss-Beams for Natural Frequency [Volume 8, Issue 1, 2011, Pages 21-28]

B

  • Bayesian Network A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine [Volume 8, Issue 2, 2011, Pages 107-117]
  • Bezier curves Midcourse Trajectory Shaping for Air and Ballistic Defence Guidance Using Bezier Curves [Volume 8, Issue 2, 2011, Pages 87-95]

C

  • Cylindrical Shell Wave Propagation Approach to Fluid Filled Submerged Visco-Elastic Finite Cylindrical Shells [Volume 8, Issue 1, 2011, Pages 57-67]

D

  • Damped natural frequencies Wave Propagation Approach to Fluid Filled Submerged Visco-Elastic Finite Cylindrical Shells [Volume 8, Issue 1, 2011, Pages 57-67]
  • Drag Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015 [Volume 8, Issue 1, 2011, Pages 1-10]
  • Dynamic coupling A Control Method Based on Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws [Volume 8, Issue 2, 2011, Pages 119-125]
  • Dynamic Response A Control Method Based on Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws [Volume 8, Issue 2, 2011, Pages 119-125]

F

  • Finite strip Method NONLINEAR POST-BUCKLING ANALYSIS OF ISOTROPIC PLATES BY USING FINITE STRIP METHODS [Volume 8, Issue 1, 2011, Pages 11-19]
  • Flight envelope Trim and Maneuverability Analysis Using a New Constrained PSO Approach of a UAV [Volume 8, Issue 1, 2011, Pages 45-56]
  • FMEA A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine [Volume 8, Issue 2, 2011, Pages 107-117]
  • Full-analytical NONLINEAR POST-BUCKLING ANALYSIS OF ISOTROPIC PLATES BY USING FINITE STRIP METHODS [Volume 8, Issue 1, 2011, Pages 11-19]

G

  • GENEX guidance Midcourse Trajectory Shaping for Air and Ballistic Defence Guidance Using Bezier Curves [Volume 8, Issue 2, 2011, Pages 87-95]

L

  • Lagrange coefficients Determination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients [Volume 8, Issue 1, 2011, Pages 37-44]
  • Least squares Determination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients [Volume 8, Issue 1, 2011, Pages 37-44]
  • LEO satellite Determination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients [Volume 8, Issue 1, 2011, Pages 37-44]
  • Lift Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015 [Volume 8, Issue 1, 2011, Pages 1-10]
  • Liquid Propellant Engine A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine [Volume 8, Issue 2, 2011, Pages 107-117]

M

  • Monte Carlo A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine [Volume 8, Issue 2, 2011, Pages 107-117]

N

  • Natural frequency A Novel Approach to Design of Truss-Beams for Natural Frequency [Volume 8, Issue 1, 2011, Pages 21-28]
  • Novel Design A Novel Approach to Design of Truss-Beams for Natural Frequency [Volume 8, Issue 1, 2011, Pages 21-28]

P

  • Particle Swarm Optimization Trim and Maneuverability Analysis Using a New Constrained PSO Approach of a UAV [Volume 8, Issue 1, 2011, Pages 45-56]
  • Pilot-Induced Oscillation A Control Method Based on Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws [Volume 8, Issue 2, 2011, Pages 119-125]
  • Pilot-Vehicle System A Control Method Based on Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws [Volume 8, Issue 2, 2011, Pages 119-125]
  • Post-buckling NONLINEAR POST-BUCKLING ANALYSIS OF ISOTROPIC PLATES BY USING FINITE STRIP METHODS [Volume 8, Issue 1, 2011, Pages 11-19]
  • Pressure Coefficient Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015 [Volume 8, Issue 1, 2011, Pages 1-10]

R

  • Reference orbit Determination of the best-fitting reference orbit for a LEO satellite using the Lagrange coefficients [Volume 8, Issue 1, 2011, Pages 37-44]
  • Reliability A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine [Volume 8, Issue 2, 2011, Pages 107-117]

S

  • Semi-analytical NONLINEAR POST-BUCKLING ANALYSIS OF ISOTROPIC PLATES BY USING FINITE STRIP METHODS [Volume 8, Issue 1, 2011, Pages 11-19]
  • Share devotion A Control Method Based on Dynamic Response of the Airplane for Compensation of Pilot-Induced Oscillations: Benefits and Flaws [Volume 8, Issue 2, 2011, Pages 119-125]
  • Spalart-Allmaras Verification of a CFD solver in near ground effect for aerodynamic behavior of airfoil NACA 0015 [Volume 8, Issue 1, 2011, Pages 1-10]

T

  • Trim-ability Trim and Maneuverability Analysis Using a New Constrained PSO Approach of a UAV [Volume 8, Issue 1, 2011, Pages 45-56]
  • Truss-beam A Novel Approach to Design of Truss-Beams for Natural Frequency [Volume 8, Issue 1, 2011, Pages 21-28]

V

  • Viscoelastic Wave Propagation Approach to Fluid Filled Submerged Visco-Elastic Finite Cylindrical Shells [Volume 8, Issue 1, 2011, Pages 57-67]
  • Von-Karman equations NONLINEAR POST-BUCKLING ANALYSIS OF ISOTROPIC PLATES BY USING FINITE STRIP METHODS [Volume 8, Issue 1, 2011, Pages 11-19]

W

  • Wave propagation approach Wave Propagation Approach to Fluid Filled Submerged Visco-Elastic Finite Cylindrical Shells [Volume 8, Issue 1, 2011, Pages 57-67]