Evaluation of FDM Rapid Prototyping with ABSi Material for Airfoil Design
-
Published:2008-08
Issue:
Volume:594
Page:249-254
-
ISSN:1662-9752
-
Container-title:Materials Science Forum
-
language:
-
Short-container-title:MSF
Author:
Daneshmand Saeed1,
Ahmadi Nadooshan A.1,
Aghanajafi C.2
Affiliation:
1. Islamic Azad University
2. K.N.Tossi University of Technology
Abstract
For faster new product introduction aerospace companies are interested in reducing the
time it takes to make wind tunnel models. The increased capability of rapid prototyping technologies
has made them attractive for this purpose. An experimental study was done of rapid prototyping
technology and their ability to make components for wind tunnel models in a timely and cost effective
manner. This paper discusses the application of wing-body-tail configuration constructed using fused
deposition method (FDM) for Subsonic and transonic wind tunnel testing. An experimental study was
undertaken comparing a rapid prototyping model constructed of FDM Technologies using ABSi
(Acrylonitrile butadiene styrene) to that of a standard machined steel model. Testing covered the
Mach range of Mach 0.3 to Mach 1.3 at an angle-of-attack range of + 4° to +26° at zero sideslip and at
angle of-sideslip ranges from –10 to +10 degrees at 16 degrees angle-of-attack.. Results from this
study show relatively good agreement between the two models. It can be concluded that FDM model
show promise in preliminary aerodynamic development studies and reduction in time and cost.
Publisher
Trans Tech Publications, Ltd.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献