Experimental Study on the Shock Oscillating in an Underexpanded Jet to Cavity Interaction Flow

碩士 === 國立成功大學 === 航空太空工程學系 === 85 === Underexpansion jet to cavity flow induced pressure oscillation inside the cavity tube and the induced temperature increasing on the bottom of the tube has been investigated based on three parameters...

Full description

Bibliographic Details
Main Authors: Wang, Chang-Nan, 王昌楠
Other Authors: Fang-Min Yu
Format: Others
Language:zh-TW
Published: 1997
Online Access:http://ndltd.ncl.edu.tw/handle/94226655554655524878