Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack

碩士 === 逢甲大學 === 機械工程研究所 === 81 ===

Bibliographic Details
Main Authors: Chen, Kuo Fang, 陳國芳
Other Authors: Lin, Albert C.Y.
Format: Others
Language:zh-TW
Published: 1993
Online Access:http://ndltd.ncl.edu.tw/handle/97481188417589717816
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spelling ndltd-TW-081FCU004890072015-10-13T17:44:42Z http://ndltd.ncl.edu.tw/handle/97481188417589717816 Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack 二維側航向量推力對後機身高攻角氣動力影響之實驗探討 Chen, Kuo Fang 陳國芳 碩士 逢甲大學 機械工程研究所 81 Lin, Albert C.Y. 林欽裕 1993 學位論文 ; thesis 0 zh-TW
collection NDLTD
language zh-TW
format Others
sources NDLTD
description 碩士 === 逢甲大學 === 機械工程研究所 === 81 ===
author2 Lin, Albert C.Y.
author_facet Lin, Albert C.Y.
Chen, Kuo Fang
陳國芳
author Chen, Kuo Fang
陳國芳
spellingShingle Chen, Kuo Fang
陳國芳
Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
author_sort Chen, Kuo Fang
title Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
title_short Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
title_full Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
title_fullStr Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
title_full_unstemmed Experimental Investigation of the Induced Aerodynamic Effects of Aftbody by 2-D Yaw-Only Thrust Vectoring at High Angle-of- Attack
title_sort experimental investigation of the induced aerodynamic effects of aftbody by 2-d yaw-only thrust vectoring at high angle-of- attack
publishDate 1993
url http://ndltd.ncl.edu.tw/handle/97481188417589717816
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