International Journal of Transportation Engineering and Technology

Special Issue

Experiments Researches in Aeronautical Engineering

  • Submission Deadline: Oct. 30, 2016
  • Status: Submission Closed
  • Lead Guest Editor: Tran Tien Anh
About This Special Issue
Aeronautical engineering involves designing aircraft such as powered lighter-than-air craft, gliders, fixed-wing airplanes and jets, autogyros, and helicopters. It is primarily involved in designing aircraft that fly within Earth's atmosphere. This special issue consists of research papers concerning specific fields of aeronautical engineering. We look forward to papers involving latest discoveries and improvements in this area.

Aims and Scope:

1. Fluid mechanics/ Aerodynamics
2. Wind tunnels testing
3. Statics and dynamics (engineering mechanics): Study of movement, forces, moments in mechanical systems.
4. Propulsion system: Energy to move a vehicle through the air is provided by internal combustion engines, jet engines and turbo machinery.
5. Control engineering: Mathematical modeling of the dynamic behavior of systems and designing them, usually using feedback signals, so that their dynamic behavior is desirable (stable, without large excursions, with minimum error). This applies to the dynamic behavior of aircraft, propulsion systems, and subsystems that exist on aerospace vehicles.
6. Aircraft structures: Design of the physical configuration of the craft to withstand the forces encountered during flight. Aerospace engineering aims to keep structures lightweight and low-cost, while maintaining structural integrity.
7. Materials science: Materials of which the aerospace structures are to be built. New materials with very specific properties are invented, or existing ones are modified to improve their performance.
8. Solid mechanics: Deals with stress and strain analysis of the components of the vehicle.
9. Aeroelasticity: the interaction of aerodynamic forces and structural flexibility, potentially causing flutter, divergence, etc.
10. Avionics: Design and programming of computer systems on board of an aircraft and the simulation of systems.
Lead Guest Editor
  • Tran Tien Anh

    Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam

Guest Editors
  • Narasimha Murty Yedidi

    Electronic Arts, Austin, United States

  • Gaurav Kumar

    Convergent Science Incorporated, New Braunfels, United States

  • Lei Kang

    Department of Civil and Environmental Engineering, University of California, Berkeley, United States

  • Cesar Vasques ORCiD

    Department of Mechanical Engineering, University of Aveiro, Aveiro, Portugal

  • Muhammad Saeed

    Department of Civil Engineering, University of Engineering and Technology, Lahore, Pakistan

  • Ly Hung Anh

    Department of Aerospace Engineering, Faculty of Transport Engineering, Ho Chi Minh City University of Technology, Vietnam National University, Ho Chi Minh City, Vietnam

  • Ngo Khanh Hieu

    Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh, Vietnam

  • Le Thi-Tuyet-Nhung

    Department of Aerospace Engineering, Ha Noi University of Science & Technology, Hai Ba Trung, Vietnam

  • Vu ngoc Bich

    Department of Science Technology - R&D, Hochiminh city University of Transportation, Vietnam

Published Articles
  • The Geometric Influence of the Tubular-Hat Tube on Its Energy Absorption Capacity in Axial Load

    Hung Anh Ly , Thanh Tien Pham

    Issue: Volume 2, Issue 4-1, December 2016
    Pages: 12-17
    Received: Aug. 12, 2016
    Accepted: Oct. 09, 2016
    Published: Nov. 22, 2016
    DOI: 10.11648/j.ijtet.s.2016020501.13
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    Abstract: Crashworthiness is an important criterion in vehicle design. In fact, a crashworthy design will reduce the terrible accidents that happen everyday. Normally, tube structures are used for this task by dissipating the impact energy on the folding waves formed during the crushing progress. This study continues the previous studies, focuses on analyzin... Show More
  • Behavior of Tubular Hat Structure Under Three Point Bending

    Le Duy Hien , Ly Hung Anh

    Issue: Volume 2, Issue 4-1, December 2016
    Pages: 18-24
    Received: Aug. 12, 2016
    Accepted: Oct. 09, 2016
    Published: Nov. 22, 2016
    DOI: 10.11648/j.ijtet.s.2016020501.14
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    Abstract: The paper focuses on the energy absorption capacity of structural materials, the most important in frame design, the structure of the vehicles, scaffolding. Main content include new solution with comparing the general structure cylinder, square tube, top-hat and reverse top-hat. After that, considering and comparing displacement, force in the trans... Show More
  • Methods of Manufacturing Aeroelasticity Bench Test for NACA0012 Wing Model in the Low Speed Wind Tunnel

    Thi Tuyet Nhung Le , Thanh Phat Duong , Nhat Truong Hoang

    Issue: Volume 2, Issue 4-1, December 2016
    Pages: 7-11
    Received: Aug. 16, 2016
    Accepted: Aug. 22, 2016
    Published: Sep. 19, 2016
    DOI: 10.11648/j.ijtet.s.2016020501.12
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    Abstract: The purpose of this study is to take measures to manufacture the experimental model: NACA 0012 wing model in the low speed wind tunnel (38 m/s). The parameters base on the achieved results of Thi-Tuyet Nhung Le & al.: “Design of aeroelasticity bench test for NACA0012 wing model in the low speed wind tunnel: Influence of wing’s parameters on flutter... Show More
  • Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5

    Ngo Khanh Hieu , Pham Quang Vinh , Dinh Anh Bao

    Issue: Volume 2, Issue 4-1, December 2016
    Pages: 1-6
    Received: Apr. 13, 2016
    Accepted: Jul. 22, 2016
    Published: Sep. 03, 2016
    DOI: 10.11648/j.ijtet.s.2016020501.11
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    Abstract: The design process of a product is a multi-step process of selection and assessment criteria to create a final product which meets all the needs of the practice. A small UAV combined between flying-wing and quadrotor is a very complex product, so the design process of this small UAV requires a thorough and circumspect review. The problem is how to ... Show More