A
-
Aerodynamic
Soft Recovery of a Supersonic Rocket using Un-Stablizing Technique [Volume 13, Issue 2, 2011, Pages 17-33]
-
Aircraft Landing Gear
The Shimmy Vibration Analysis of Aircraft Landing Gear [Volume 13, Issue 2, 2011, Pages 59-69]
-
Aviation Accident
Identifying the effective factors in aviation accident and providing an appropriate model [Volume 13, Issue 2, 2011, Pages 71-78]
-
Aviation Safety
Identifying the effective factors in aviation accident and providing an appropriate model [Volume 13, Issue 2, 2011, Pages 71-78]
B
-
Boundary element method
Boundary Integral Equations for Time Domain Solution and Reduced Order Modeling of Thin Wings Unsteady Aerodynamics [Volume 13, Issue 1, 2011, Pages 39-51]
C
-
Civil Airplane
Experimental and Numerical Investigation of Vortex Generator effects on Flow Pattern and Aerodynamic Coefficients of an Airplane Wing Model [Volume 13, Issue 2, 2011, Pages 1-16]
-
Combustion chamber
A 3-D study of primary holes geometry effectiveness on film cooling efficiency and thrust of combustion chamber [Volume 13, Issue 2, 2011, Pages 35-47]
F
-
Film Cooling
Application of Turbulence Model in Investigation of Film Cooling Problem over a Flat Plate [Volume 13, Issue 1, 2011, Pages 53-62]
-
Flight dynamic
Soft Recovery of a Supersonic Rocket using Un-Stablizing Technique [Volume 13, Issue 2, 2011, Pages 17-33]
-
Flow Pattern
Experimental and Numerical Investigation of Vortex Generator effects on Flow Pattern and Aerodynamic Coefficients of an Airplane Wing Model [Volume 13, Issue 2, 2011, Pages 1-16]
G
-
Gas Turbines
Application of Turbulence Model in Investigation of Film Cooling Problem over a Flat Plate [Volume 13, Issue 1, 2011, Pages 53-62]
-
Graph theory
The Design and Calculation of Hydraulic Networks of Cooled Turbine Blades of the Jet Engine Using Graph Theory [Volume 13, Issue 1, 2011, Pages 63-73]
H
-
H∞ loop shaping
Autopilot Design using Static H∞ Loop shaping controller [Volume 13, Issue 2, 2011, Pages 79-94]
-
Human factor
Identifying the effective factors in aviation accident and providing an appropriate model [Volume 13, Issue 2, 2011, Pages 71-78]
L
-
Laminates
Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method [Volume 13, Issue 1, 2011, Pages 87-97]
-
Limit Cycle Oscillation
The Shimmy Vibration Analysis of Aircraft Landing Gear [Volume 13, Issue 2, 2011, Pages 59-69]
-
Linear and Nonlinear Analysis
The Shimmy Vibration Analysis of Aircraft Landing Gear [Volume 13, Issue 2, 2011, Pages 59-69]
M
-
Miner's rule
Life Estimation of a Helicopter Main Rotor Shaft Based on Standard FAA Spectrum [Volume 13, Issue 2, 2011, Pages 49-58]
-
M-K theory
A New Approach in Predicting the Extent of Thin Plates Formation [Volume 13, Issue 1, 2011, Pages 76-85]
O
-
Optimal control
Development of a Mushy State Simulated Annealing Algorithm for the Design of an Optimal Path Regulator Autopilot System [Volume 13, Issue 1, 2011, Pages 23-37]
P
-
Parallelism
Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method [Volume 13, Issue 1, 2011, Pages 87-97]
R
-
Robust autopilot
Autopilot Design using Static H∞ Loop shaping controller [Volume 13, Issue 2, 2011, Pages 79-94]
S
-
Semnan Model
Identifying the effective factors in aviation accident and providing an appropriate model [Volume 13, Issue 2, 2011, Pages 71-78]
-
Shimmy Vibration
The Shimmy Vibration Analysis of Aircraft Landing Gear [Volume 13, Issue 2, 2011, Pages 59-69]
-
Simulated Annealing
Stiffness Optimization of Laminates based on a modified Parallel Simulated Annealing method [Volume 13, Issue 1, 2011, Pages 87-97]
-
Soft recovery
Soft Recovery of a Supersonic Rocket using Un-Stablizing Technique [Volume 13, Issue 2, 2011, Pages 17-33]
-
SST and κ-ω turbulence models
Application of Turbulence Model in Investigation of Film Cooling Problem over a Flat Plate [Volume 13, Issue 1, 2011, Pages 53-62]
-
Static controller
Autopilot Design using Static H∞ Loop shaping controller [Volume 13, Issue 2, 2011, Pages 79-94]
-
Supersonic
Soft Recovery of a Supersonic Rocket using Un-Stablizing Technique [Volume 13, Issue 2, 2011, Pages 17-33]
T
-
Thrust
A 3-D study of primary holes geometry effectiveness on film cooling efficiency and thrust of combustion chamber [Volume 13, Issue 2, 2011, Pages 35-47]
-
Turbulence model
Application of Turbulence Model in Investigation of Film Cooling Problem over a Flat Plate [Volume 13, Issue 1, 2011, Pages 53-62]
-
Turbulent Flow
Application of Turbulence Model in Investigation of Film Cooling Problem over a Flat Plate [Volume 13, Issue 1, 2011, Pages 53-62]
U
-
Unsteady Aerodynamics
Boundary Integral Equations for Time Domain Solution and Reduced Order Modeling of Thin Wings Unsteady Aerodynamics [Volume 13, Issue 1, 2011, Pages 39-51]
V
-
Vortex Generator
Experimental and Numerical Investigation of Vortex Generator effects on Flow Pattern and Aerodynamic Coefficients of an Airplane Wing Model [Volume 13, Issue 2, 2011, Pages 1-16]
W
-
Weights optimization
Autopilot Design using Static H∞ Loop shaping controller [Volume 13, Issue 2, 2011, Pages 79-94]
-
Wind tunnel test
Experimental and Numerical Investigation of Vortex Generator effects on Flow Pattern and Aerodynamic Coefficients of an Airplane Wing Model [Volume 13, Issue 2, 2011, Pages 1-16]
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