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Journal of Aerospace Engineering & Technology Cover

Journal of Aerospace Engineering & Technology

E-ISSN: 2231-038X | P-ISSN: 2348-7887 | Peer-Reviewed Journal (Refereed Journal) | Hybrid Open Access

About the Journal

Journal of Aerospace Engineering & Technology Journal of Aerospace Engineering & Technology (JOAET) is a peer-reviewed hybrid open-access journal launched in 2011, focused on the rapid publication of fundamental and multidisciplinary research papers on all areas of Aerospace Engineering & Technology.

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Journal Metrics

Key performance indicators showcasing our journal’s impact and reach

36

Published Articles (2024)

20.05

Days Acceptance Time

46.6

Day Publication Time

Total Visits

Journal Information

Title: Journal of Aerospace Engineering & Technology
Abbreviation: joaet
Issues Per Year: 3 Issues
P-ISSN: 2348-7887
E-ISSN: 2231-038X
Publisher: STM Journals, An imprint of Consortium e-Learning Network Pvt. Ltd.
DOI: 10.37591/JoAET
Starting Year: 2011
Subject: Aerospace Engineering
Publication Format: Hybrid Open Access
Language: English
Copyright Policy: CC BY-NC-ND
Type: Peer-reviewed Journal (Refereed Journal)

Address:

STM Journals, An imprint of Consortium e-Learning Network Pvt. Ltd. A-118, 1st Floor, Sector-63, Noida, U.P. India, Pin - 201301

Editorial Board

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joaet maintains an Editorial Board of practicing researchers from around the world, to ensure manuscripts are handled by editors who are experts in the field of study.

Editor in Chief

Editor

Dr. Dilip A. Shah, Senior Professor and Dean

Hindustan University, Chennai, India,

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Latest Articles

Ahead of Print

AI-Assisted Optimization of Supersonic Airfoil Shapes Using CFD Coupling

This paper presents a novel framework for optimizing supersonic airfoil geometries through integrated artificial intelligence and computational fluid dynamics coupling.

Supersonic aerodynamics, Airfoil optimization, Computational fluid dynamics, Neural network surrogate, Particle swarm optimization, Drag reduction, High-speed flow.

Design and Development of a Mini Drone for Educational Applications

This paper describe the complete process of designing, building, and testing a small unmanned aerial vehicle (UAV), normally referred to as a drone.

Mini Drone, brushless DC motors, lithium-polymer

Design of Maritime Empennage Unmanned Aerial Vehicle (UAV): A Comprehensive Study

This project presents a comprehensive study on the design and development of a maritime empennage unmanned aerial vehicle (UAV) tailored for operations in coastal and naval environments.

Maritime Empennage, Aerial Vehicle, Aerodynamic

The Decision of the Maximum Synchronous Torque During the Solar Array Deployment Using the Closed Cable Loop

It was a long time since mankind explored and studied the universe, but the early-age power sources have not changed a lot over that period. Solar panels have been used long ago and are still in use today.

Solar array, deployment, multi-DOF dynamic model, synchronous torque, linkage

A Study on Unmanned Air Vehicles (UAV)

Unmanned Air Vehicles (UAVs), commonly known as drones, represent one of the most transformative technologies of the 21st century, rapidly evolving from their initial military applications into a diverse array of civilian and commercial uses.

Unmanned air vehicle, military, agriculture, communication, infrastructure, safety

Robust Design of Subsonic Airfoil by Multi-Objective Six Sigma Approach

It is well known that aerodynamic performance of a UAV is very sensitive to the wing shape and flight conditions, and inevitable uncertainties such as wing manufacturing errors and wind variations may lead to drastic deterioration in its aerodynamic performance.

Airfoil, robust design, multi-objective six sigma analysis, lift to drag ratio, spline approximation