A
-
Analysis
Optimum design of the turbine blisk of a mini-turbojet engine [Volume 4, Issue 1, 2015, Pages 83-98]
-
Artificial neural network
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2015, Pages 77-94]
C
-
Control
Guidance and control system design for an aerial robot based on reference trajectory acceleration [Volume 4, Issue 1, 2015, Pages 17-31]
E
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Engine Rotational Speed
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2015, Pages 77-94]
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Exhaust Gas Temperature
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2015, Pages 77-94]
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Experimental Micro Gas Turbine Engine
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2015, Pages 77-94]
G
-
Guidance
Guidance and control system design for an aerial robot based on reference trajectory acceleration [Volume 4, Issue 1, 2015, Pages 17-31]
-
Gurney flap designing
Aerodynamic improvement of oscillating airfoils efficiency at low Reynolds number by using of Gurney flaps [Volume 4, Issue 1, 2015, Pages 47-55]
H
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Heat Transfer Dynamics
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
M
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Modeling
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2015, Pages 45-54]
-
Modeling
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
-
Multiple-Polynomial Regression
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2015, Pages 77-94]
N
-
Noise
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2015, Pages 45-54]
-
Numerical method
The effect of the damage on the aerodynamic characteristics of wing with respect to the three-dimensional effects [Volume 4, Issue 2, 2015, Pages 7-19]
P
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Piezoelectric layers
Robust active vibration suppression of a nonlinear flexible spacecraft [Volume 4, Issue 2, 2015, Pages 35-44]
R
-
RANS turbulence models
Prediction of flow separation in a low-pressure turbine cascade at design and off-design operating conditions [Volume 4, Issue 1, 2015, Pages 57-69]
S
-
Sensitivity
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2015, Pages 45-54]
-
Shaft Dynamics
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
-
Simulink
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
-
Smith Predictor
Attitude control system design for a clustered launch vehicle in the presence of vibration in direct sub-band space [Volume 4, Issue 1, 2015, Pages 7-16]
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Stress intensity factors
Determination of mixed mode stress intensity factors for longitudinally seam weld pipes containing 3D semi elliptical cracks [Volume 4, Issue 1, 2015, Pages 71-82]
T
-
Turbojet
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
V
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Vibration Control
Attitude control system design for a clustered launch vehicle in the presence of vibration in direct sub-band space [Volume 4, Issue 1, 2015, Pages 7-16]
-
Volume Dynamics
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2015, Pages 65-76]
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