A
-
Abbasi, Yousef
Guidance and control system design for an aerial robot based on reference trajectory acceleration [Volume 4, Issue 1, 2015, Pages 17-31]
-
Abdolahi Poor, Soheila
The effect of the damage on the aerodynamic characteristics of wing with respect to the three-dimensional effects [Volume 4, Issue 2, 2016, Pages 7-19]
-
Arabi, Hoseyn
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
B
-
Badrrezayi, Hoseyn
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
-
Basohbat Novinzadeh, Alireza
Guidance and control system design for an aerial robot based on reference trajectory acceleration [Volume 4, Issue 1, 2015, Pages 17-31]
-
Bazazzadeh, Mehrdad
Evaluation of wing vortex behavior at high angles of attack by using laser visualization and numerical method [Volume 4, Issue 2, 2016, Pages 21-33]
-
Beiki, Alireza
Aerodynamic improvement of oscillating airfoils efficiency at low Reynolds number by using of Gurney flaps [Volume 4, Issue 1, 2015, Pages 47-55]
-
Bohlouri, Vahid
Development of a systematic design approach for a cubic Satellite using design structure Matrix method [Volume 4, Issue 1, 2015, Pages 33-45]
D
-
Dehghan Manshadi, Mojtaba
Evaluation of wing vortex behavior at high angles of attack by using laser visualization and numerical method [Volume 4, Issue 2, 2016, Pages 21-33]
E
-
Ebrahimi, Hoseyn
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
-
Eilbeigi, Mehdi
Evaluation of wing vortex behavior at high angles of attack by using laser visualization and numerical method [Volume 4, Issue 2, 2016, Pages 21-33]
F
-
Fakoor, Mehdi
Development of a systematic design approach for a cubic Satellite using design structure Matrix method [Volume 4, Issue 1, 2015, Pages 33-45]
-
Farahbakhsh, Hassan
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]
-
Faraji, Mohamad
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2016, Pages 65-76]
-
Feizian, Mehdi
Evaluation of wing vortex behavior at high angles of attack by using laser visualization and numerical method [Volume 4, Issue 2, 2016, Pages 21-33]
H
-
Habibnia Rami, Mehdi
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]
J
-
Jahromi, Mehdi
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2016, Pages 65-76]
K
-
Karamooz, Mohammad Reza
Optimum design of the turbine blisk of a mini-turbojet engine [Volume 4, Issue 1, 2015, Pages 83-98]
-
Khoshnood, Abdol Majid
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]
-
Kosari, Amir reza
Development of a systematic design approach for a cubic Satellite using design structure Matrix method [Volume 4, Issue 1, 2015, Pages 33-45]
L
-
Lamei, Saeed
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2016, Pages 45-54]
M
-
Mahmoodi, Mostafa
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2016, Pages 65-76]
-
Malekzadeh, Maryam
Robust active vibration suppression of a nonlinear flexible spacecraft [Volume 4, Issue 2, 2016, Pages 35-44]
-
Mani, Mahmoud
The effect of the damage on the aerodynamic characteristics of wing with respect to the three-dimensional effects [Volume 4, Issue 2, 2016, Pages 7-19]
-
Mirhabibi, Ali Reza
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
-
Mohammad Aliha, Mohammad Reza
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]
-
Mohammadi, Masoud
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]
-
Moosavian, Seyed Ali Akbar
Guidance and control system design for an aerial robot based on reference trajectory acceleration [Volume 4, Issue 1, 2015, Pages 17-31]
N
-
Naderi, Alireza
Aerodynamic improvement of oscillating airfoils efficiency at low Reynolds number by using of Gurney flaps [Volume 4, Issue 1, 2015, Pages 47-55]
-
Nakhodchi, Soheil
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
-
Navid Ghoreishi, Seyed Mohammad
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]
P
-
Pirkandi, Jamasb
Parametric analysis of transient performance of a turbojet engine based on nonlinear aero-thermodynamic modeling approach [Volume 4, Issue 2, 2016, Pages 65-76]
R
-
Riazi, Roozbeh
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]
-
Riazi, Roozbeh
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2016, Pages 77-94]
S
-
Sadeghi, Mohammad
An experimental investigation in effects of thermal fatigue and constant bending loading on failure of a sample of thermal barrier coatings [Volume 4, Issue 2, 2016, Pages 55-64]
-
Shahriari, Behrooz
Optimum design of the turbine blisk of a mini-turbojet engine [Volume 4, Issue 1, 2015, Pages 83-98]
-
Sheibani, Ayoob
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]
-
Siami, Majid
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2016, Pages 45-54]
T
-
Tajdari, Mehdi
Optimum design of the turbine blisk of a mini-turbojet engine [Volume 4, Issue 1, 2015, Pages 83-98]
-
Tarvirdizadeh, Bahram
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2016, Pages 77-94]
V
-
Vakilipour, Shidvash
Development of a systematic design approach for a cubic Satellite using design structure Matrix method [Volume 4, Issue 1, 2015, Pages 33-45]
-
Vakilipour, Shidvash
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]
-
Vakilipour, Shidvash
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2016, Pages 77-94]
-
Veisi, Hadi
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2016, Pages 77-94]
Y
-
Yousefi, Shahram
Optimum design of the turbine blisk of a mini-turbojet engine [Volume 4, Issue 1, 2015, Pages 83-98]
Z
-
Zakeri, Manigheh
Modeling of a lateral comb capacitive micro accelerometer system behavior for 1g acceleration [Volume 4, Issue 2, 2016, Pages 45-54]
-
Zare, Hadi
Using statistical and artificial intelligence approach to predict the exhaust gas temperature of a micro gas turbine engine [Volume 4, Issue 2, 2016, Pages 77-94]
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