Wing-in-ground-effect craft: A case study in aerodynamics

  • Authors

    • Surjatin Wiriadidjaja
    • Amzari Zhahir
    • Zahratu Hilall Mohamad
    • Shikin Razali
    • Ahmad Afifi Puaat
    • Mohamed Tarmizi Ahmad
    2018-10-09
    https://doi.org/10.14419/ijet.v7i4.13.21319
  • wing-in-ground-effect, WIGE craft, aerodynamics, ekranoplan, hoverwing.

  • Abstract

    A wing-in-ground-effect (WIGE) crafts can be deployed to fly by utilizing the ground effect, which is a natural phenomenon known to improve the efficiency of airplanes during take-off and landing approaches. In contrast, WIGE craft is not commercially viable for public transport mainly due to the difficulties in controlling its longitudinal stability. As an attempt to support the development of WIGE crafts, this paper presents a case study in aerodynamics based on certain published reports, specifically to reveal the available research data that are considered of interest and can be used as a lesson for further study and analysis. The wind tunnel procedure and testing, as well as numerical investigation of a WIGE craft, are applied and the results are then analyzed. The discussions are oriented in the perspectives of aerodynamics. Based on the tests and calculation, parameters concerning the ground effect as the WIGE crafts approaching the ground surfaces may be identified and hence their values can be determined. Thus, the static longitudinal stability may then be established and optimized for control of the WIGE craft.

     

     

  • References

    1. [1] Wiriadidjaja S, Mohamad ZH, Mohd Rafie AS, Elhadi M, Fariduzzaman & Hasim F (2016), Wing-in-ground-effect craft as a potential domestic transport vehicle. AIAA Applied Aerodynamics Conference

      [2] Wieselsberger C (1922), Wing resistance near the ground. NASA-TM-77

      [3] Curry RE, Moulton BJ & Kresse J (1989), An in-flight investigation of ground effect on a forward-swept wing airplane of the X-29A. NASA TM-101708

      [4] Wayne MO & Colgren RD (2003), Ground effect determination of a Piper Comanche. AIAA Atmospheric Flight Mechanics Conference and Exhibit

      [5] Earl TD (1962), Ground effect machines. AGARDograph

      [6] Mineck RE (1974), Effect of ground proximity on the longitudinal aerodynamic characteristics of an aspect-ratio-1 wing with and without wing-tip blowing. NASA-TM X-3048

      [7] Griffith CD & Skutecki ER (1986), VTOL Altitude Hold System with Automatic Ground Effect Compensation, Patent US4603388 A

      [8] Boeing (2002), Pelican Ultra Large Transport Airplane. http://www. boeing.com/news/frontiers/ archive/2002/september/i_pw.html

      [9] Kartik A (2005), Prediction of dynamic ground effect forces for fixed wing airplane. Patent US20050197811 A1

      [10] Novikov-Kopp I (2011), Method for comprehensively increasing aerodynamic and transport characteristics, a wing-in-ground-effect craft. Patent US20110266081 A1

      [11] Yin CM, Wiriadidjaja S, Majid DLA, Romli FI, Rafie ASM & Zhahir A. (2015), Review on the cost and performance of a WIGE craft: A commercialization prospective. ARPN Journal of Engineering and Applied Sciences 10(21), 10027-10033

      [12] Nebylov AV & Nebylov VA (2014), Controlled WIG flight concept. 19th World Congress of the International Federation of Automatic Control

      [13] Nebylov A & Nebylov V (2008), WIG-craft marine landing control at rough sea. 17th World Congress of the International Federation of Automatic Control

      [14] Nebylov A (2008), Wing-in-ground effect flight control: New role of automatic systems. World Congress of the International Federation of Automatic Control

      [15] Nebylov A (2014), Wing-in-ground effect vehicles flight automatic control systems development problems. Applied Mechanics and Materials 629, 370-375

      [16] Anderson N & Nolte W (2005), Systems engineering principles applied to basic research and development. Georgia Tech Space Systems Engineering Conference

      [17] Kossiakoff A, Sweet WN, Seymour SJ & Biemer SM (2011), Systems Engineering Principle and Practice. John Wiley & Sons, Inc.

      [18] Collinson RPG (1996), Introduction to Avionics. Springer

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  • How to Cite

    Wiriadidjaja, S., Zhahir, A., Hilall Mohamad, Z., Razali, S., Afifi Puaat, A., & Tarmizi Ahmad, M. (2018). Wing-in-ground-effect craft: A case study in aerodynamics. International Journal of Engineering & Technology, 7(4.13), 5-9. https://doi.org/10.14419/ijet.v7i4.13.21319

    Received date: 2018-10-08

    Accepted date: 2018-10-08

    Published date: 2018-10-09