A
-
Aerodynamic coefficients
Investigation of Airfoil Oscillation on Aerodynamic Coefficients with an Accurate Algorithm [Volume 1, Issue 1, 2013, Pages 12-19]
-
Air Trafic
Equipping Boeing 707 Airplane with RVSM System and Uncertainty Analysis of Altimeter System [Volume 1, Issue 1, 2013, Pages 31-39]
-
Altimeter
Equipping Boeing 707 Airplane with RVSM System and Uncertainty Analysis of Altimeter System [Volume 1, Issue 1, 2013, Pages 31-39]
-
Attitude control
Design of an Attitude Controller for Large-Angle Maneuvers of a Satellite considering of Reaction Wheels Constraints with High Fidelity Model [Volume 1, Issue 1, 2013, Pages 20-30]
B
-
Blowing ratio
Investigation of Velocity Ratio Difference between the Controlling Jets and the Main Jet in the Compound Triple Jets Arrangement to Modify the Film Cooling Effectiveness, Using the LES Approach [Volume 1, Issue 1, 2013, Pages 2-11]
-
Buckling
Numerical and experimental investigations on buckling of steel cylindrical shells with various cutouts [Volume 1, Issue 1, 2013, Pages 62-69]
C
-
Compositeshell
Nonlinear Vibration Analysis Of Clamped-Clamped Composite Cylindrical Shells [Volume 1, Issue 1, 2013, Pages 52-61]
-
Cutout
Numerical and experimental investigations on buckling of steel cylindrical shells with various cutouts [Volume 1, Issue 1, 2013, Pages 62-69]
-
Cylindrical Shells
Numerical and experimental investigations on buckling of steel cylindrical shells with various cutouts [Volume 1, Issue 1, 2013, Pages 62-69]
F
-
FEM
Numerical and experimental investigations on buckling of steel cylindrical shells with various cutouts [Volume 1, Issue 1, 2013, Pages 62-69]
-
Finite Volume Element Method
Investigation of Airfoil Oscillation on Aerodynamic Coefficients with an Accurate Algorithm [Volume 1, Issue 1, 2013, Pages 12-19]
-
Flight Test
Equipping Boeing 707 Airplane with RVSM System and Uncertainty Analysis of Altimeter System [Volume 1, Issue 1, 2013, Pages 31-39]
G
-
Galerkin’s method
Nonlinear Vibration Analysis Of Clamped-Clamped Composite Cylindrical Shells [Volume 1, Issue 1, 2013, Pages 52-61]
L
-
Lagrangian-Eulerian Approach
Investigation of Airfoil Oscillation on Aerodynamic Coefficients with an Accurate Algorithm [Volume 1, Issue 1, 2013, Pages 12-19]
-
Large-Angle Maneuvers
Design of an Attitude Controller for Large-Angle Maneuvers of a Satellite considering of Reaction Wheels Constraints with High Fidelity Model [Volume 1, Issue 1, 2013, Pages 20-30]
-
Large Eddy Simulation Approach
Investigation of Velocity Ratio Difference between the Controlling Jets and the Main Jet in the Compound Triple Jets Arrangement to Modify the Film Cooling Effectiveness, Using the LES Approach [Volume 1, Issue 1, 2013, Pages 2-11]
M
-
Modalmethod
Nonlinear Vibration Analysis Of Clamped-Clamped Composite Cylindrical Shells [Volume 1, Issue 1, 2013, Pages 52-61]
N
-
Non-Linearequation
Nonlinear Vibration Analysis Of Clamped-Clamped Composite Cylindrical Shells [Volume 1, Issue 1, 2013, Pages 52-61]
S
-
Smagorinsky Model
Investigation of Velocity Ratio Difference between the Controlling Jets and the Main Jet in the Compound Triple Jets Arrangement to Modify the Film Cooling Effectiveness, Using the LES Approach [Volume 1, Issue 1, 2013, Pages 2-11]
U
-
Uncertainty
Equipping Boeing 707 Airplane with RVSM System and Uncertainty Analysis of Altimeter System [Volume 1, Issue 1, 2013, Pages 31-39]
V
-
Vertical Separation Minimum
Equipping Boeing 707 Airplane with RVSM System and Uncertainty Analysis of Altimeter System [Volume 1, Issue 1, 2013, Pages 31-39]
-
Vibration
Nonlinear Vibration Analysis Of Clamped-Clamped Composite Cylindrical Shells [Volume 1, Issue 1, 2013, Pages 52-61]
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