The Design and Discussion of a Micro Gas Turbine Engine

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 91 === The micro gas turbine engine has a good potential for UAV propulsion and power generation applications. Whereas the turbine engine with thrust level below 1 lbf is non-exist, except the MIT micro turbine made by MEMS technology. The objective of the present...

Full description

Bibliographic Details
Main Authors: Yau-Cheng Li, 李曜丞
Other Authors: Chen, Shih-Hsiung
Format: Others
Language:en_US
Published: 2003
Online Access:http://ndltd.ncl.edu.tw/handle/02227925917156344683

Similar Items