Numerical simulation for forebody/inlet integration flowfield of supersonic tactical missile using PNS methods

博士 === 中正理工學院 === 國防科學研究所 === 79 ===

Bibliographic Details
Main Authors: PENG,JIAN-WEN, 彭健文
Other Authors: XU,YAN
Format: Others
Language:zh-TW
Published: 1991
Online Access:http://ndltd.ncl.edu.tw/handle/54420097896512841538