Keyword Index

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]

T

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]