File:NLC416-08jh003213-22755 簡易空氣動力學.pdf

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簡易空氣動力學   (Wikidata search (Cirrus search) Wikidata query (SPARQL)  Create new Wikidata item based on this file)
Author
〔美〕柯雷鳴(A.Klemin)著
image of artwork listed in title parameter on this page
Title
簡易空氣動力學
Publisher
商務印書館[發行] ([長沙])
Description

目錄
第一章 幾種有用之數學及力學原理
常數
算式之變形
幾何學及三角學中之問題
三角函數之數值
飛機攀升之例題
速度之圖解法
相對速度及速度之加法
力,合力,與分力
重心及力矩
力與加速度
功與功率

習題
答案
第二章 空氣與大氣之性質
空氣之性質
標準空氣
標準大氣
由溫度及壓力計算空氣密度法
實用例題
習題
第三章 流線流及白諾禮氏定律
完美流體與流線流
白諾禮氏定律
白氏定律之一般的應用
白氏定律在空氣動力學中之應用
飛行時可假設空氣為不可壓縮之氣體
機翼上升力之解釋
第四章 飛行之基本原理
飛行之基本原理
相對運動原理
與風向垂直之平面所受之阻力對於密度,面積及速度之關係
重量,質量,比重及密度
動量,加速度及力
阻力定律之數學的證明
與風向垂直之平面上所受之阻力
空氣動力變化之普遍定律
仰角
翼展,翼弦及展弦比
升力係數與阻力係數
升力與阻力之比
合力及壓力中心
習題
第五章 機翼周圍之氣流及機翼測驗法
曲面何以較平面為優
機翼周圍之氣流因機翼之傾斜度而變更
風洞測力法
機翼周圍壓力之分布
平面機翼之性質
標準機翼剖面之性質
機翼之升力,阻力與速度之關係
習題
答案
第六章 飛機性能之基本計算法─飛機,螺旋槳及發動機之配合
機翼馬力
clarky剖面之特性表
機翼阻力及機翼馬力圖線
寄體阻力及寄體馬力之圖線
總阻力與總馬力之圖線
總阻力及總馬力之直接計算法
平板面積當量
飛機之總效率
可用馬力之計算法
標準發動機之馬力轉數圖線
飛機螺旋槳之基本原理
螺旋槳效率計算法
螺距之意義
飛機攀升時發動機轉速減低之原因
攀升時之螺旋槳效率何以較在最高速度時為小
可用功率圖線計算法
螺旋槳之更換法
金屬螺旋槳之優點
習題
答案
第七章 飛機力學綱要
滑翔
滑翔降落小場法
倒垂下沖
穩定平飛時之平衡
習題
答案
第八章 飛機力學綱要(續)─轉彎
離心力
物體轉彎時必需用力以抵抗離心力
偏側轉彎時之力的平衡
駕駛人在高速之峭立偏側飛行時失去知覺之原因
偏側指示器
錯誤之偏側
轉彎時所需之速度及功率較直飛時為大
轉彎學習法
操縱面
習題
答案
第九章 飛機力學綱要(續)─轉彎
因副翼而生之偏航動向
自然偏側力矩開始轉彎與持續轉彎
轉彎之簡單法則
內側滑及外側滑
發動機轉動力矩之效果
峭立側飛時操縱機關作用之改變
習題
答案
第十章 落地及落地奔程
落地時之突躍現象
完美之三點落地
低速落地之優點
關於落地速度應注意之點
急行落地
與落地奔程有關之因子
制動器對於飛機設計之影響
風之影響
四周有障礙物之機場何以必須較大
問題
第十一章 起飛及攀升
起飛時飛機所受之力
平滑地面上之起飛
粗糙地面上之起飛
正確之起飛
如何使起飛迅速
逆風起飛
最佳之攀升
最峭立之攀升
順風攀升與逆風攀升
攀升時之失速
習題
第十二章 縱方安定性
力學上之安定實例
只有機翼之飛機必不安定
平尾面何以能使飛機安定
翻旋力矩之定義
飛機安定性之計算法
調穩飛機於固定之仰角法
習題
答案
第十三章 縱方安定性(續)
風洞對於研究縱方安定性之用途
重心位置前後對於安定性之影響
重心位置高低對於安定性之影響
改變安定面角度之影響
飛機平衡上之缺點不能用安定面之角度改正之
滑流效果及推力線位置
寄體阻力對平衡之影響
實際飛行之平衡測驗
動力安定性
縱方平衡之實用修正法
強大之安定性及強大之控制
習題
答案
第十四章 橫方安定性
作單純側滾時實無安定性
側滾時必有內側滑
直翅,二面角及掠後
偏航時之安定
側滑,偏航及側方急風之效果相同
側滾時之阻尼現象及飛機之自動旋轉
完美橫方安定所需之條件
第十五章 現代之翼面學說
旋轉圓柱何以能升起
翼面升力之循環氣流論
翼梢渦流
翼梢渦流之另一解釋
翼展上各點皆有渦流
翼梢渦流可生誘導阻力
用渦動說解釋展弦比之效果
習題
答案
第十六章 翼剖面選擇法
翼剖面應有之性質
優良翼剖面應有之條件
流體動力學與翼剖面
幾種代表的翼剖面之分析
對各表之討論
r.a.f.15
clarky
gottingen387
習題
答案
第十七章 伯吉氏氣隙與其他增加機翼升力之裝置
單翼變作雙翼法
可變曲度之機翼
面積及曲度雙變之機翼
可變之配角
襟翼
旋轉圓柱
翼面氣層之操縱
伯吉氏氣隙
固定氣隙之效果小
氣隙與襟翼必須並用之理由
關於氣隙之最新成績
自動氣隙
將來氣隙必能通用
第十八章 雙翼機之空氣動力學
雙翼機與單翼機之比較
雙翼上之各種定義
雙翼渦流論淺釋
雙翼效率之計算法
直疊雙翼之特性
掩錯
掩錯及配角差
平均空氣動力弦
兩翼上載荷之分配
習題
第十九章 寄體各部之阻力及飛機全體之空氣動力學
圓柱之阻力
串列線纜之阻力
流線形張線支柱之阻力
機身阻力
發動機之遮罩法
自由空氣散熱器之阻力
尾面阻力
輪之阻力
減少寄阻之可能方法
習題

Language Chinese
Publication date 民國29[1940]
Source
institution QS:P195,Q732353
(民國時期文獻 民國圖書)
主題
InfoField
航空學:空氣動力學 空氣動力學:航空學
中圖分類
InfoField
V211
拼音題名
InfoField
jian yi kong qi dong li xue
載體形態
InfoField
274頁

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