File:NLC416-11jh003598-54934 日本九六式艦上戰鬥機之研究.pdf

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日本九六式艦上戰鬥機之研究   (Wikidata search (Cirrus search) Wikidata query (SPARQL)  Create new Wikidata item based on this file)
Author
吳有榮著
image of artwork listed in title parameter on this page
Title
日本九六式艦上戰鬥機之研究
Publisher
正中書局
Description

分3章：構造說明、性能計算、結論。有王士倬序，著者序。附日本九七式陸上戰鬥機構造簡述等4種

目錄
王序
自序
三面圖
設備圖
第一章 構造說明
第二章 性能計算
第一節 測得數
第二節 機翼特性
第三節 阻力之估計
第四節 海平面飛行性能
第五節 高空飛行性能
第六節 特種飛行性能
第七節 海平面最高平飛速度之縱向安定性
第八節 臨界高度最高平飛速度之橫向安定性
第九節 性能摘要
附圖 （目次詳下頁）
第三章 結論
附錄一 日本九七式陸上戰門機構造簡述（附三面圖）
附錄二 符號說明
附妹三 航空工程常用各表
甲 航空工程常用液體黏度表
乙 航空工程常用液體之近似密度表
丙 航空工程常用度量衡換算表
一 長度l
二 面積l²
三 容積及容量l³
四 速度l/t
五 衡量f
六 壓力f/l²
七 工能fl
八 工率fl/t
九 質量密度f/e/（l/t）²
十 密度f/l²
附錄四 中英文術語對照表
附圖目次
0 圖ii1a 翼根剖面(日本九六式艦上戰關機）
1 圖ii2a 美國航空諮議會翼剖面圖解
2 圖ii2b 無升力襲角
3 圖ii2c 機巽升力係數對襲角曲線之斜度
4 圖ii2d 機翼最小阻力係數
5 圖ii2e 機翼阻力係數對開力係數平方曲線之斜度
6 圖ii2f 繞機翼氣動力心不變力矩係數
7 圖ii2g 機翼最大升力係數
8 圖ii2h naca 2412翼部面之模型比例及擾流對最大升力系圖ii2i數之效果
9 圖ii2i 英國皇家航空隊raf30 翼部面表皮粗細對最大升力係數之效果
10 圖ii2j 展弦比b為clmax及cdu之函數
11 圖ii2k af對100℅翼展分裂式襟翼之機翼效果
12 圖ii2l 100℅翼展及45º襟翼角之襟翼翼弦對機翼待性之效果
13 圖ii2m 20℅翼弦及60º翼角之襟翼翼展對機翼特性之
14 圖ii2n 空氣動力黏度倒數
15 圖ii2o 克拉克（clark)翼剖面之漠型比例及攏流對無升力襲角之效果
16 圖ii2p 擾流對dcl/da及dcd/dcl²之效果
17 圖ii2q 單翼機展弦比與升力係數對制角曲線之斜度關係
18 圖ii2r 克拉克（clark)y翼剖面表皮阻力對其最小陰力係數之比較
19 圖ii2s 機翼阻力係數對升力係數平方曲線之斜度為展弦比之函數
20 圖ii3x 機身及船身阻力與俯仰角之關係
21 圖ii3b 相當於平板之飛機寄生阻力面積
22 圖ii4a 金屬螺旋槳在整流之發動機及機翼前之效率及v/nd對c
23 圖ii4b 油門開足後金屬螺旋槳可發出之馬力對飛機速度
24 圖ii5a 油門開足無增壓器發動機金屬螺旋槳可發出之馬力於不變空速正對飛行高度之關係
25 圖ii6a 螺旋槳靜推力係數
26 圖ii6b 最大升力與阻力比可為寄生阻力及展弦比之函
27 圖ii6c 起飛時間及距離之係數
28 圖ii6d 迎風起飛之滑駛距離
29 圖ii6e 旋飛時各力平穩圖解
30 圖ii6f 無風降落距離
31 圖ii7a 機翼力距圖解
32 圖ii8a 翼面負荷對全機縱轉動慣量因數a
33 圖ii8b 翼面負荷對全機豎轉動慣量因數c
34 圖ii8c 翼寬及側滾力心圖解
35 圖一 指示速度對馬力（日本九六艦戰機）
36 圖二 上升速率地高度（日本九六艦戰機）

Language Chinese
Publication date 民國31[1942]
Source
institution QS:P195,Q732353
(民國時期文獻 民國圖書)
館藏信息
InfoField
MG/E926.392
主題
InfoField
軍用飛機 軍用飛機 艦載飛機
中圖分類
InfoField
E926.392
載體形態
InfoField
74頁

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