Volume 7 (2023)
Volume 6 (2022)
Volume 5 (2021)
Volume 4 (2020)
Volume 3 (2019)
Volume 2 (2018)
Volume 1 (2017)
Number of Volumes 8
Number of Issues 30
Number of Articles 188
Number of Contributors 349
Article View 96,314
PDF Download 44,132
View Per Article 512.31
PDF Download Per Article 234.74
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Number of Submissions 352
Reject Rate 27
Accepted Submissions 188
Acceptance Rate 53
Number of Indexing Databases 12
Number of Reviewers 422

The Journal of Technology in Aerospace Engineering (JTAE), is a quarterly scientific double-blind peer-reviewed publication concerned with appropriate aspects of Air and Space engineering. Technology in Aerospace Engineering (JTAE) is an open-access publication, which publishes original research Articles, Scientific extension, and research notes. 

Technology in Aerospace Engineering (JTAE), has obtained a publishing license and has obtained scientific-research validity with license letter No. 133118/18/3 dated 25/02/2019 of the Ministry of Science, Research and Technology.

Publication Fee: article processing charge and any other publication fees in the Journal of Technology in Aerospace Engineering are free for authors.
Subscription Fee: Journal of Technology in Aerospace Engineering is no subscription fee for audiences.

Review Time is a maximum three months from receipt to acceptance.   

Bibliography Method: IEEE , EndNote 

The Journal of Technology in Aerospace Engineering (JTAE) also follows the Committee on Publication Ethics (COPE) Regulations. 

All submitted manuscripts are checked for similarity through a trustworthy software named Hamanandjo software to be assured about its originality and then rigorously peer-reviewed by the international reviewers.

the Journal of Technology in Aerospace Enginnering is licensed under a " Creative Commons Attribution License (CC BY)

Having an ORCID identifier is mandatory for all authors. You can register at https://orcid.org/register.

 


 

Scientific extension Aerodynamics/Fluid Mechanics/Aeroacoustics/...
Investigating selected methods to improve aerodynamic coefficients and better performance of UAV

Mohamad hossein Moghimi Esfandabadi; Mohammad Hassan Djavareshkian

Volume 8, Issue 3 , September 2024, Pages 1-16

https://doi.org/10.22034/jtae.2024.8.3.1

Abstract
  An unmanned aircraft (UAV) is a type of aircraft that operates without the need for a human passenger. These planes are able to fly automatically, without the need for remote control, and are mostly controlled by computers and sensors. UAVs are used in many industries and have various applications, including ...  Read More

Research Article Propulsion/Thermodynamics/Heat Transfer/Fuel and Combustion/Energy/...
Design of cryogenic propulsion feeding system for second stage of special rocket Based on space standards

MohamadAmin Borghei; Muhammad Amin Eskandari

Volume 8, Issue 3 , September 2024, Pages 17-32

https://doi.org/10.22034/jtae.2024.8.3.2

Abstract
  In general, according to the Russian Gost standard, the space propulsion engine system includes injection subsystems, thrust chamber, heat transfer and cooling system, launch system, feeding system, thrust vector control system which due to overlap and penetration The manifolds between the engine reservoirs ...  Read More

Research Article Space Engineering/Space Orbit Mechanics/Space Sciences/...
Adaptive Modified Sliding-Mode-based Attitude Control of a Satellite Under Reaction Wheel Fault

Narges Talebi Motlagh; Sevil Mohammadzadeh Sadigh; hossein beheshti; hamid Ghouchi Eskandar; Moharram Shameli

Volume 8, Issue 3 , September 2024, Pages 33-46

https://doi.org/10.22034/jtae.2024.8.3.3

Abstract
  In this paper, passive adaptive modified sliding-mode-based fault tolerant control is designed to track the desired attitude of a satellite with four reaction wheels in the presence of external disturbances, system uncertainties, and actuator fault. In order to achieve this goal, the adaptive modified ...  Read More

Research Article Propulsion/Thermodynamics/Heat Transfer/Fuel and Combustion/Energy/...
Analysis and identification of the flow pattern in a specific high-pressure axial turbine in off-design conditions

Sahar Saharkhiz; Reza Aghaei Togh

Volume 8, Issue 3 , September 2024, Pages 47-61

https://doi.org/10.22034/jtae.2024.8.3.4

Abstract
  The aim of this research is to identify the flow pattern in off-design conditions of a specific high-pressure axial turbine. by writing the preliminary design code, the turbine was designed, Then the geometry of this turbine was designed in CATIA and Ansys Design Modeler softwares, and it is meshed in ...  Read More

Research Article Space Engineering/Space Orbit Mechanics/Space Sciences/...
conceptual design of store and forward payload for LEO satellite

elham hosseini; razieh Narimani

Volume 8, Issue 3 , September 2024, Pages 63-74

https://doi.org/10.22034/jtae.2024.8.3.5

Abstract
  One of the satellite telecommunication services is the S&F service. In this article, we analyze the service characteristics and explain the impact of them on the design parameters. One of the challenges of telecommunication payload design is the mapping of service parameters to the technical requirements ...  Read More

Scientific extension Flight mechanics/Navigation/Control/...
A review of the application of optimization algorithms nature inspired in the design of flight paths

Iman Shafieenejad; Mohammadreza Banitalebi Dehkordi; Mohammad Amin Nourianpour

Volume 8, Issue 3 , September 2024, Pages 75-99

https://doi.org/10.22034/jtae.2024.8.3.6

Abstract
  In this article, an overview of the application of optimization algorithms inspired by nature in the design of the flight path has been discussed. The significant increase in the capabilities and availability of independent ground and air tools makes safety and security challenges especially important ...  Read More

Costs of the Aircraft Fleet Design, Construction and Operation in the Islamic Republic of Iran

hussain gharehbaghi

Volume 1, Issue 2 , December 2017, , Pages 55-62

Abstract
  Due to the problems in the country (Islamic Republic of Iran) for purchasing aircraft and aircraft old fleet, a solution should be proposedfor this problem. One way to address this need is designing and manufacturing the aircraft in the country.According to the previous investigations carried out, 180-seater ...  Read More

Methods and Tools: Computational (CFD)/Measurement (Experimental)/Analytical (Mathematical)/...
Three-Dimensional Lbm Simulation of Oscillations of a Pendent ‎Growing Drop‎

Shahram Ghorbanifar; M. Taeibi Rahni; M. Zareh

Volume 5, Issue 1 , May 2021, , Pages 67-77

https://doi.org/10.22034/jtae.2021.135091

Abstract
  In this work, the force-displacement equation and non-linear three-dimensional oscillations of a pendant drop are investigated numerically. The presented novel force-displacement function allows following the dynamics of a pendant drop and realizing its elastic behavior. The growth and detachment of ...  Read More

Aerodynamics/Fluid Mechanics/Aeroacoustics/...
Methods for Attenuation of Helicopter

Hamid Parhizkar; Ali Moradi; Alireza Hejazi zade

Volume 7, Issue 3 , September 2023, , Pages 69-84

https://doi.org/10.30699/jtae.2023.7.3.6

Abstract
  Helicopters can be a source of loud noise. The high production noise of helicopters makes them unsuitable for densely populated areas, especially in low-flying conditions. This study examines methods and offers solutions to reduce or eliminate the noise produced by helicopters. Several methods have been ...  Read More

Aerodynamics/Fluid Mechanics/Aeroacoustics/...
Design and optimization of the wing fence of a lambda-shaped aircraft model to reduce the rolling moment coefficient

Mohammad hossein Moghimi Esfandabadi; Mohammad Hassan Djavareshkian

Volume 8, Issue 2 , June 2024, , Pages 13-25

https://doi.org/10.22034/jtae.2024.8.2.2

Abstract
  This research investigates the effect of fence on wingtip vortices and control surfaces in a bird-like aircraft using numerical methods. In designing and placing the fence, average dimensions extracted from wing root vortices at different angles of attack have been used. In addition, the fence with specified ...  Read More

Structure/Solid Mechanics/Solid Dynamics/Vibrations/Aeroelasticity/...
Free vibration analysis of cylindrical sandwich shells with FML face and functionally graded core using a new shell theory

Ali Davar; Mohsen Heydari Beni; Reza Azarafza; Jafar Eskandari Jam

Volume 7, Issue 4 , January 2024, , Pages 35-49

https://doi.org/10.30699/jtae.2023.7.4.4

Abstract
  In this research, by improving the accuracy of existing high-order theories, a new corrected high-order composite cylindrical shell theory with twelve displacement components has been developed. In this theory, the effect of terms related to the trapezoidal shape of the shell cross-section (1+z/R) in ...  Read More

Research Article Structure/Solid Mechanics/Solid Dynamics/Vibrations/Aeroelasticity/...
Investigating the effect of wear on the creepage life of jet engine turbine blades model 250-C20

Mostafa Livani; Hamid Reza Zarei; Seyed Mohammad Kamali

Articles in Press, Accepted Manuscript, Available Online from 24 January 2024

Abstract
  The fixed and moving blades of turbines in the hot part of jet engines and turboshafts, due to bearing extreme stresses at high temperature, are constantly exposed to various damages and failures such as hot corrosion, oxidation, creep damage, erosion, fatigue foreign body damage, and cracking. On the ...  Read More

Research Article Flight mechanics/Navigation/Control/...
Two-Level Optimal Controller Design Based on PSO and Adaptive Control for Satellite Simulator System

Alireza Ahangarani Farahani; Reza Yaghoi; Seyed Majid Hosseini

Articles in Press, Accepted Manuscript, Available Online from 29 January 2024

Abstract
  In this paper, to control the Euler angles of a three-degree-of-freedom satellite simulator platform with uncertain parameters an adaptive inverse dynamic control method based on the PSO algorithm is presented. The design of the controller is done in two steps, in the first step, the control coefficients ...  Read More

Scientific extension Life Sciences/Environment/Plant Physiology/Animal Physiology/Remote Sensing/...
Plant Research in Space Shuttle and its Challenges

Halimeh Hassanpour

Articles in Press, Accepted Manuscript, Available Online from 19 February 2024

Abstract
  The study of plant growth and development during spaceflight is very important in promoting fundamental and applied biological knowledge as well as the life support system.The purpose of this study was to investigate the scientific and technical aspects of plant experiments and designed hardware for ...  Read More

Research Article Flight mechanics/Navigation/Control/...
Design of robust sliding mode controller for nonlinear chaotic gyroscope system with input saturation

Ali Foroutan; Alireza Safa

Articles in Press, Accepted Manuscript, Available Online from 21 January 2024

Abstract
  The gyroscope system is an attractive and efficient nonlinear system that is used in various military, aerospace, navigation, and many other important industries. In this paper, a robust sliding mode controller is proposed to control the chaotic gyroscope nonlinear system in the presence of noise, external ...  Read More

Research Article Aviation/Piloting/Flight Care/Safety/Standard/Avionics/Air Telecommunications/...
Analytical Study of Mutual Inductance for Arbitrary Positioned Planar Spiral Inductors for Airborne Electromagnetic Systems Applications

Ata Ollah Mirzaei,; َAmir Mosa Abazari; Hamed Ghanbarpour; Mahdi Asadi; Hadi Tavakkoli

Articles in Press, Accepted Manuscript, Available Online from 21 January 2024

Abstract
  The calculation of mutual inductance has widespread applications in microelectromechanical systems (MEMS) sensors and wireless power transfer in microchips. Flat coil structures are commonly employed for implementing coils in micro dimensions. MEMS sensors and microchips with flat coil structures have ...  Read More

Research Article Flight mechanics/Navigation/Control/...
Air target tracking by homing missile using deep learning and fuzzy adaptive control

mohamad mahdi soori; seyed hosein Sadati

Articles in Press, Accepted Manuscript, Available Online from 29 January 2024

Abstract
  In the integrated guidance and control approach, the guidance law is developed separately and tested assuming the ideality of the autopilot. The autopilot is also designed independently and is tested assuming the ideality of the guidance law. This article describes the process of designing and simulating ...  Read More

Research Article Aerodynamics/Fluid Mechanics/Aeroacoustics/...
Experimental study of the aerodynamics of micro airfoils with wavy surface and the use of different patterns inspired by nature

Mehdi Abedi; Ramin Zakeri

Articles in Press, Accepted Manuscript, Available Online from 18 May 2024

https://doi.org/10.22034/jtae.2024.1337

Abstract
  In this research, which was carried out experimentally and in the wind tunnel, the effect of corrugation of Naca 0012 airfoil on its aerodynamic characteristics has been studied. After the tests, the wavy airfoil at 15,000 and 66,000 Reynolds showed a very good aerodynamic performance compared to the ...  Read More

Research Article Structure/Solid Mechanics/Solid Dynamics/Vibrations/Aeroelasticity/...
Thermomechanical Buckling Analysis of Rectangular Piezoelectric Sandwich Microplates

Mostafa Livani; Mohammad Rajaei; Vahid Khalafi

Articles in Press, Accepted Manuscript, Available Online from 18 May 2024

https://doi.org/10.22034/jtae.2024.1335

Abstract
  Abstract: This article studies the thermomechanical buckling behavior of a sandwich honeycomb rectangular microplate with simply supported boundary conditions under thermal loading and applied voltage . The model studied consists of two piezoelectric layers of barium titanate and an aluminum honeycomb ...  Read More

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