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发表于 2008-3-7 09:17:08
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来自: 中国山东泰安
目录
目录
$ V# _$ m6 ]' V% F0 q0 ^7 o3 f8 b5 [第一章绪论....................................................................1
K8 X! `6 B1 V! b' ^" ?1.1本课题研究背景.....................................................................................................15 p! A& r2 `# ]6 t; {& z) Y
1.2国内外研究技术现状............................................................................................. 2/ B9 ?) o; q% o, m' \
1.3本课题研究内容........................................................................................................ 2
8 V* c$ r t$ p& c( X: \' S第.章基本概念与基本原理............................................................................................... 5
. p& n6 {3 Y- L8 u$ A2.1翼型结构基本概念............................................................................................5
7 t! m, c) J& f0 i9 \ 2.1.1翼型几何参数....................................................................................................5
* C# _0 v& @7 t( b9 P. Q 2.1.2翼型介绍................................................................................................7
! v" m# v6 D+ Z0 C1 D& V3 H( Z! s: j2.2翼型空气动力学相关概念......................................................................:....................... 78 O) V: `. P3 H& H
2.2.1作用在翼型上的空气动力........................................................................................ 7" w! W; U) x1 i6 e5 ~
2.2.2空气动力的影响因素................................................................................................ 9
|+ x* }- s# \, x9 i5 j# v n5 Z7 o5 D2.3叶片基本气动理论..............................................................................................11; ^/ O# G, U2 L
2.3.1贝兹理论...................................................................................................................115 T3 t. M& m/ }+ f p; X
2.3.2涡流理论..........................................................................................13! b4 o$ }" g, ?& g, M+ l7 ]8 f
2.3.3叶素理论.................................................................................................14
( A8 \0 k- Z, r: V 2.3.4动量理论.........................................................................................................16, H. F8 B& j! j! o2 V8 J, w
2.4本章小结................ ................................................................................17
3 `, k0 z2 d9 t3 D$ M4 G第三章叶片设计.......................:...............................................18
1 H6 c6 f. h8 `1 e. X/ V3.1前言.......................................................................................................188 S& B1 j9 M9 `& m, G
3.2风力机特征风速的确定............................................................................................18
9 O% f. r2 e' @( G B, s; w {4 W 3.2.1风速的数学表达式..............................................................................................18
3 F, r8 @2 J; U, k 3.2.2风力机特征风速的推导计算.................................................................................. 20. Z: V' [7 _8 `( }1 T) R( d$ E# H
3.3叶片基本设计方法....................................................................................................21
% z6 b2 \+ q4 I* x% y' ~+ s& o9 O 3.3.1计算风轮直径模型..........................................................................................219 t9 Q5 l1 x5 L5 X* i' Q
3.3.2叶片重要参数的选取.............................................................................................. 23
9 {1 i9 P# a+ S- P广西大学ZXt学位论文
. q9 p& J- Y9 R. g. l% G8 E风办发电机叶t卜iR计研究, F7 ^1 N0 m" |
3.3.3叶展形状设计模型..............................................................................................25
9 ?" n- \/ e o" A" E q* ]9 ?3.4叶片设计实例.................................................................................................29
6 ]' @! ?4 c. U 3.4.1风力机特征风速的确定.......................................................................................... 29/ b% n z4 U2 P* o
3.4.2叶片重要参数选取..............................................................................................30: t% L K: c3 g* h) C
3.4.3叶展形状设计...................:..........................................................................32 l1 l l9 L/ B
3.5设计结果形象化................................................................................................41( ^9 q3 z5 u; p, ^# n2 r
3.5.1叶片截面空间坐标的求解...................................................................................... 41
& W: }4 O8 y& c& p7 A# T 3.5.2叶片计算机3D绘图............................................................................................... 44: {* I! v7 w9 K0 C! T3 [, V% Q
3.5.3该3D建模方法的优点........................................................................................... 45
9 ?. w% V U. ~, t: f; e, `3.6叶片模型图......................................................................................................... 46% c0 l6 X1 r9 U; i r: _/ e( F
3.7本章小结................................................................................................................47
. [' Q; {0 L/ Y% E第四章静态气动性能模拟计算........................:.............................. 484 x+ ] x8 W2 {3 r
4.1前言.......................................................................................................484 C( D0 B) `, [8 \* ]
4.1.1有量纲性能指标...................................................................................................... 48
" X* F# G- l2 T9 x+ E/ B. [% f 4.1.2无量纲性能指标、..................................................................................................... 48
( H% t3 _0 [! G5 x$ x* Q- B 4.1.3有量纲指标和无量纲指标关系......................................................................48* y4 c, e: V$ F5 X8 I* M6 x
4.2叶片气动性能计算...............................................................................................49% {( Y/ u: y1 R9 s% A3 X8 x
4.2.1贝茨模型..........................................................................................................492 `1 n- O& }; Z T
4.2.2涡流模型—Glauert模型和Wilson模型.................................................49* Y1 R4 ~7 v; s7 Q7 z d) Q# t2 C
4.3各种修正系数..............................................................................................54* U# K4 s1 z1 S; R! W* {' e
4.3.1叶片数修正...................................................................................54
& S, {* w. f! l% b9 l 4.3.2翼型修正....................................................................................................55/ \9 D- T8 x, T
4.3.3叶尖修正..........................................................................................................55
: z/ G! |% q$ R+ p- r$ [ 4.3.4轮毅修正..............................................................................................................56
6 V! \/ {9 ], o4.4模型修正结果................................................................................................56
_# z- W/ j$ B4 N 4.4.1性能修正表..........................................................................................................570 w+ K" A, N9 S- T3 k4 n$ f
4.4.2结果分析..........................................................................................................60
' H0 ?7 ~& o9 _# ]3 U( l# d! c4.5本章小结........................................................................................................................ 61, G# e2 A/ X* ]3 E5 o( `
第五章叶片动力学分析........................................................... 62& x* G& R# k$ f$ L. p$ W
广西大学祠盯士学位金仑.弋
0 O- P& z1 t/ c2 s9 u/ g$ m5 X" Z风办发电机叶少卜宝又计笼开乡t
- j6 p! y% J3 E( q) P5.1前言............................................................................................................62
: ?3 ^5 Y5 O9 Y9 x5.2动力学分析方法............................................................................................................ 62/ g$ v; w& V' s# |- d
5.3计算模型................................................................................................................63
$ E/ f3 N/ t: V7 t* t5.4分析工具................................................................................................................63
; H h5 ?7 R; }& H5 W) l x* }5.5分析步骤.............................、.............................................................................651 }5 c$ V" _+ Y( y' @+ W: L5 Z+ l. s
5.5.1有限元建模.............................................................................................................. 65
2 t; c9 r' N1 L- I p) X; J" j0 l 5.5.2施加约束..........................................................................................................67
1 x3 O8 _" W& A" m; [8 o5.6计算结果........................................................................................................67
- B+ ]' \8 u V# O; j- M, p( U7 W2 u7 {8 H 5.6.1模态计算结果..................................................................................................67" E3 |( }. A* h# `5 F+ |
5.6.2结果分析..............................................................................................................68
5 S) H7 N, Z. u" X5 A4 t 5.6.3对比计算.................................................................................................................. 725 N# V7 }3 D3 Q- y/ Q! A" C
5.6.4计算模型的改进...................................................................................................... 74# j& c G- }6 O8 E$ ]- Q% u0 d* k
5.6.5结论..................................................................................................................74
+ q, @. X* \* G5.7本章小结................................................................................................................74
, G/ Z# W+ {* B6 R备第六章结论及展望................................................................................ 76
( e A: V5 d [# \/ g9 @5 Y8 Z6.1结论....................................................................................................................76* J$ E7 m: T; \$ d" d; x5 K' e
6.2论文堕待解决的问题.................................................................................................... 77
8 P' K7 J/ M9 y7 d8 R7 A. t6.3展望..................................................................................................................77& @, j; D! Y7 s
参考文献.......................................................................:..78$ m" I2 q/ N* z4 N* ?" I1 y. P
附录1翼型NACA4412数据.....................................................829 O9 `: V H9 G7 L% z
附录2翼型NACA4412气动性能表(RE=500000) ............................................................ 83
% {! z! U6 w, K0 _4 @$ R: J附录3翼型NACA4412气动性能图(RE=500000) ................................................. 848 m9 j# ~* Y- e# w6 ]# h8 k
致谢.......................................................................................................... 85
6 I$ h8 C) a3 T9 K7 z/ n攻读学位期间发表的学术论文目录................................................................................... 86 |
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