Volume 14 (2021)
Volume 13 (2020)
Volume 12 (2019)
Volume 11.1 (2018)
Volume 11 (2017)
Volume 10 (2013)
Volume 9 (2012)
Volume 8 (2011)
Volume 7 (2010)
Volume 6 (2009)
Volume 5 (2008)
Volume 4 (2007)
Volume 3 (2006)
Volume 2 (2005)
Volume 1 (2004)
Number of Volumes 16
Number of Issues 38
Number of Articles 257
Number of Contributors 434
Article View 171,600
PDF Download 44,324
View Per Article 667.7
PDF Download Per Article 172.47
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Accepted Submissions 294
Acceptance Rate 52
Time to Accept (Days) 137
Number of Indexing Databases 3
Number of Reviewers 253

It is my pleasure to introduce this new journal in aerospace science and technology. As we understand, there is little or no forum in this field with an international scope in the region of central and west Asia, and therefore we strongly believe that it will make it possible in the region and in the whole world for better communication among scientists and researchers in aeronautical and astronautical sciences and technologies, and also in all related fields as aerodynamics and fluid mechanics, thermodynamics and propulsion, combustion and heat transfer, dynamics and control, flight mechanics, design, structures and vibration, aviation management, etc.

Publication order: bi-quarterly

Language: English

The ethical policy of JAST is based on the Committee on Publication Ethics (COPE) guidelines and complies with the Committee of JAST's Editorial Board codes of conduct.

All articles published in the journal are in a state of free access for the public to study or scientific exploit in accordance with the principles of research and correct citing.

 

Aerospace Science and Technology
1. Mixed Mode (I/II/III) Stress Intensity Factors in Gas Turbine Blade Considering 3D Semi-elliptical Crack

Seyed mohammad navid ghoreishi; Nabi Mehri-Khansari; Houman rezaei

Volume 15, Issue 1 , June 2022, Pages 1-13

http://dx.doi.org/10.22034/jast.2021.294317.1077

Abstract
  Regardless of the initiation or propagation procedure of crack in a gas turbine blade, the precise expectation of the fracture behavior, such as mixed-mode Stress Intensity Factors (SIF), plays a significant role in acquiring its operational life. Therefore, multilateral three-dimensional fracture solutions ...  Read More

Aerospace Science and Technology
2. Numerical study on enhancement of low speed axial compressor rotor performance under radial inlet distortion via DBD plasma actuators

Ali Khoshnejad; Reza Ebrahimi; Golamhosein Pouryossefi

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2021.309899.1102

Abstract
  Aero-engine entrance conditions are not always ideal and, for various reasons, inlet distortion may occur and cause inlet blockage and reduction of compressor performance. The aim of this study was to numerically simulate the effects of plasma actuators on the enhancement of low-speed axial compressor ...  Read More

Aerospace Science and Technology
3. Numerical calculation of radiation heating of the hypersonic nose in the reentry phase

Sajad Ghasemlooy; mahsa dehnamaki; Hamid Parhizkar

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2021.300023.1089

Abstract
  The calculation of aerodynamic heating is one of the most important steps in designing high speed flying bodies, especially reentry bodies. Because ignoring that, it can damage the thermal protection system and cut off the radar connections to the reentry capsule. Due to the high speed of the capsule ...  Read More

Aerospace Science and Technology
4. Sliding mode stabilization of quad tilt-wing UAV considering nonlinear model of the vehicle and uncertainties

Mahdi Amani Estalkhkuhi; Jafar Roshanian

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.296063.1086

Abstract
  In this paper, a multi-input/multi-output sliding controller is proposed and analyzed for a quad tilt-wing unmanned aerial vehicle (QTW-UAV). The vehicle is equipped to do take-off and landing in vertical flight mode and is capable of flight over long distances in horizontal flight mode. The full dynamic ...  Read More

Aerospace Science and Technology
5. Developement of Vision-Based Human Tracking for Drone’s Gimbal

Mohammad Hossein Bayat; Mohammad Shahbazi; Bahram Tarvirdizadeh

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.312829.1105

Abstract
  The use of Unmanned Aerial Vehicles (UAVs) with different features and for a variety of applications has grown significantly. Tracking generic targets, especially human, using the UAV's camera is one of the most active and demanding fields in this area. In this paper we implement two vision-based tracking ...  Read More

Aerospace Science and Technology
6. Simulation of the effect of using a finned tube on the thermal efficiency of a Helicopter shell and tube heat exchanger.

Mohammad Reza Salimi; Mohsen Rostami; Amir Hamzeh Farajolahi; Morteza Ghanbari

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.317457.1108

Abstract
  In this paper, flow and heat transfer inside a helicopter shell and tube heat exchanger is simulated in three dimensions. This converter consists of a shell with 90 U-shaped tubes inside. For further heat transfer, the tubes were simulated and compared once without fins and again with fins, which are ...  Read More

Aerospace Science and Technology
7. Development of real-time aeroelastic flight simulation tool for primary design and stability analysis

Hossein Favaedi

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.246477.1036

Abstract
  Flight simulation is a powerful and usefull instrument in design, testing, evaluation and validation of aircrafts; The results of aerolastic simulation along with rigid simulation can be used in the many areas of designs, such as modification or optimization, stability analysis and evaluating field test ...  Read More

Aerospace Science and Technology
8. Design process of a supersonic wind-tunnel working with vapor of combined cycle power plant

hossein shadmehr; Sajad Ghasemloo; hamid Parhizkar

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.297517.1087

Abstract
  In this article, the idea of building a supersonic wind tunnel has been provided that uses a high-pressure steam flow of a combined cycle power plant. This has been investigated by CFD method. Using the plant's output steam as a high-pressure source can be used in the ejector to create supersonic airflow ...  Read More

Aerospace Science and Technology
9. natural periodic orbit attitude behavior of satellites in three-body problem in the presence of the oblate primaries

Amir reza Kosari; Ehsan Abbasali; Majid Bakhtiyari

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.311711.1104

Abstract
  The main purpose of this article is to examine the periodic coupled orbit-attitude of a satellite at restricted three body problem considering both primaries oblateness perturbations. The proposed model was based on a simplified coupled model meaning that the time evolution of the orbital state variables ...  Read More

Aerospace Science and Technology
10. Noise-Induced Miss Distance Analysis of First-Order Explicit Guidance Law

Ali Arabian Arani; S.H. Jalali Naini; mohammad hossein Hamidi nejad

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.303074.1095

Abstract
  This study presents the miss distance analysis of the first-order explicit guidance law due to seeker noise using the adjoint method. For this purpose, linearized equations are utillized and the adjoint model is developed. Then the first-order equations are obtained and converted into nondimensional ...  Read More

Aerospace Science and Technology
11. Adaptable Nonlinear Guidance Law Design with Respect to Initial Deviation for Booster Vertical Landing Mission

Morteza Sharafi; Nasser Rahbar; Ali Moharrampour; Abdorreza Kashaninia

Volume 15, Issue 1 , June 2022

http://dx.doi.org/10.22034/jast.2022.327899.1113

Abstract
  In this study, terminal phase guidance of a vertical-landing booster has been considered. At first, dynamical equations have been derived assuming variable mass, density and gravity model. Then by considering these parameters as constants, sensitivity variables have been extracted using the vectorized ...  Read More

Aerospace Science and Technology
1. Numerical and Experimental Analysis of Ballistic Behaviour of Ceramic-Reinforced Al Matrix Composite Plates

Ali Ansari; Jafar Eskandari Jam; Ali Alizadeh; Mohsen Heydari Beni; Majid Eskandari Shahraki

Volume 13, Issue 2 , October 2020, , Pages 7-26

http://dx.doi.org/10.22034/jast.2021.126370

Abstract
  This study was designed to investigate the ballistic behavior of ceramic-reinforced aluminum composite plates numerically and experimentally and to present an optimal sample design. The parameters studied were ceramic reinforcement percentage and type of matrix alloy. This study used the matrix alloys ...  Read More

Aerospace Science and Technology
2. Analysis of Composite Lattice Cylindrical Shells Under Transient Dynamic Loading

Ali Davar; Mahdi Mehrabani; MohammadReza Zamani; Mohsen Heydari Bani; Jafar Eskandari Jam

Volume 14, Issue 1 , June 2021, , Pages 30-44

http://dx.doi.org/10.22034/jast.2021.133431

Abstract
  The composite lattice cylindrical shells are analyzed in this research while they are subjected to transient dynamic loading. The equilibrium equations for the composite cylindrical shell are expressed in terms of classical shell theory. Additionally, due to the discontinuous distribution of stiffness ...  Read More

Aerospace Science and Technology
3. Investigation of Flow Separation Phenomenon for Supersonic Convergent–Divergent Nozzles

Omid Habibi; Reza Ebrahimi; Hassan Karimi Mazraeh Shahi

Volume 14, Issue 2 , October 2021, , Pages 141-151

Abstract
  The nozzle, an end-element of the propulsive process Cycle, represents a critical part of any aerospace vehicle. The task of accelerating and efficiently exhausting combusted and reactive gases according to the delivered thrust represents the main objective of the propulsion system design. Flow separation ...  Read More

Aerospace Science and Technology
4. Design of Multi-Input Multi-Output Controller for an Unmanned Aerial Vehicle by Eigenstructure Assignment Method

Ali Motamedi; Abolghasem Naghash

Volume 14, Issue 1 , June 2021, , Pages 117-127

http://dx.doi.org/10.22034/jast.2021.133347

Abstract
  The purpose of this paper is to present a Multi-Input Multi-Output (MIMO) linear controller based on the eigenstructure assignment method for a fixed-wing Unmanned Aerial Vehicle (UAV) in longitudinal and lateral-directional channels. To this end, a six degree-of-freedom model of the aerial vehicle is ...  Read More

Aerospace Science and Technology
5. Restricted Three-Body Problem Considering Perturbations of Oblate Primaries

Ehsan Abbasali; Amir reza Kosari; Majid Bakhteiari

Volume 13, Issue 2 , October 2020, , Pages 27-35

http://dx.doi.org/10.22034/jast.2021.128013

Abstract
  In this paper, the effect of perturbations of oblate primaries in the Circular Restricted Three-Body Problem is studied, and the equations of satellite orbital motion in the Circular Restricted Three-Body Problem are developed by employing Lagrangian mechanics. Since the equations have no closed-form ...  Read More

Aerospace Science and Technology
1. Droplet Breakup Analysis inside Porous Media at Different Porosities, Using LBM

Mohammad Reza Salimi; Mohammad Taeibi Rahni; Abolfazl Amiri Hezaveh

Articles in Press, Accepted Manuscript, Available Online from 10 April 2022

http://dx.doi.org/10.22034/jast.2022.322220.1110

Abstract
  In present research, the interaction between single liquid droplet with particles inside a porous media is investigated numerically in two dimensions. The He’s model is used to simulate two phase flow and multiple relaxation time collision operator is implemented to increase numerical stability. ...  Read More

Aerospace Science and Technology
2. Three-Axis Satellite Attitude Control with Fractional-Order PID Controller in the presence of Uncertainty and Disturbance

Amir reza Kosari; Elahe Khatoonabadi; Vahid Bohlouri

Articles in Press, Accepted Manuscript, Available Online from 13 April 2022

http://dx.doi.org/10.22034/jast.2022.321251.1109

Abstract
  In this paper, the control of a three-axis rigid satellite attitude control system with a fractional order proportional-integral-derivative (PID) controller is investigated in the presence of disturbance and parametric uncertainties. The reaction wheel actuator with the first-order dynamic model is used ...  Read More

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