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]