Design and Fabrication of a Winged Hybrid Airship Model for IIUM-LSWT-Reference-Cited by-同舟云学术

Design and Fabrication of a Winged Hybrid Airship Model for IIUM-LSWT

Published:2015-07 Issue: Volume:1115 Page:513-516
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

Ul Haque Anwar¹,Amri Hafiz Nik Mohamad¹,Kashif S.M.¹,Asrar Waqar²,Omar Ashraf Ali³,Sulaeman Erwin¹,Ali J.S. Mohamed²

Affiliation:

1. International Islamic University Malaysia

2. International Islamic University Malaysia (IIUM)

3. University Of Tripoli

Abstract

Wind Tunnel Testing on a subscaled model of a winged hybrid airship requires a faithful reproduction of all geometric details of actual airship. Due to huge volume of hull, geometrical parameters of such airships are quite different from that of an aircraft. In this article, a scheme for designing such models is described alongwith a review of different strategies available for manufacturing of its prototype wind tunnel model in IIUM low speed wind tunnel. Similar to aircrafts, major contributing factors for scaling, design and manufacturing of a subscaled model of hybrid airships are discussed. It is concluded that the required aerodynamic data will be the dictating factor for selection of the manufacturing method.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.1115.513.pdf

Reference10 articles.

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2. Burnett, D., Kammeyer, M., Berry, C. & Larach, E., Experiences in fabrication of a waverider model for wind tunnel testing, AIAA (1993).

3. Pope, A. Harper, J, J., Low speed wind tunnel testing, John Wiley & Sons, New York, (1966).

4. Pankhurst, R, C. Holder, D, W., Wind-tunnel techniques: an account of experimental methods in low and high speed wind tunnels, Pitman, London, (1952).

5. Wind-tunnel model Systems Criteria, NASA Report No. LPR 1710. 15, January 28, (2009).

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