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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
) A4 o/ e+ n/ G$ \第一章绪论....................................................................1
2 R) _; l( `1 P. z. Q; c1.1本课题研究背景.....................................................................................................18 L3 `5 R1 o% x. u/ {/ r1 v; i) Q6 R
1.2国内外研究技术现状............................................................................................. 27 d# n0 B i4 X5 Z3 r
1.3本课题研究内容........................................................................................................ 2
0 y7 Y% C& y' V+ t H5 s第.章基本概念与基本原理............................................................................................... 5
+ p0 Q) ]6 m4 R% B' x& O2.1翼型结构基本概念............................................................................................52 \. ?- \+ s' s, ?
2.1.1翼型几何参数....................................................................................................50 }# Z! J( n, }
2.1.2翼型介绍................................................................................................7
1 [+ k. I I" C" ]4 e; b @; l+ H2.2翼型空气动力学相关概念......................................................................:....................... 79 F' E$ m7 r: z8 I; X0 _% V
2.2.1作用在翼型上的空气动力........................................................................................ 7
" E! {8 A4 o" e/ F Z. d 2.2.2空气动力的影响因素................................................................................................ 9
' I2 n5 D, k. e+ N, x6 ~2.3叶片基本气动理论..............................................................................................11
2 S% H. E1 s9 u# K 2.3.1贝兹理论...................................................................................................................11
' v. Q/ N4 V4 ^4 ~! } 2.3.2涡流理论..........................................................................................13
1 N% Q( ?* a" b" z' D* z8 V 2.3.3叶素理论.................................................................................................14' ^, U; q. F$ w- w, Y5 z. P
2.3.4动量理论.........................................................................................................16
A# b( A) Y' q2.4本章小结................ ................................................................................172 n; p/ Z, H( `# o
第三章叶片设计.......................:...............................................18
; V F- a. [0 G( h$ v, L3.1前言.......................................................................................................18, d& ^# b7 ?% a# m% F& V8 W
3.2风力机特征风速的确定............................................................................................18
% o5 R/ r; R6 b3 J 3.2.1风速的数学表达式..............................................................................................18; E+ N5 Z5 O0 p, }# S3 ^: ?" L
3.2.2风力机特征风速的推导计算.................................................................................. 20, @8 k: v- L4 _8 `& I, |
3.3叶片基本设计方法....................................................................................................21+ \( X2 y# d* g/ d) H4 b
3.3.1计算风轮直径模型..........................................................................................21
- e0 x3 b: L& W1 r' C8 g) _ 3.3.2叶片重要参数的选取.............................................................................................. 23) w; m; B) c3 M
广西大学ZXt学位论文
& Z6 C( K7 I( z4 ^3 O- n风办发电机叶t卜iR计研究- E# i' i$ \* l& X5 l: r# ~
3.3.3叶展形状设计模型..............................................................................................25
+ Z; Z4 {. \7 V' x# i3.4叶片设计实例.................................................................................................29
+ B4 C1 ?/ H' t9 U4 R) f2 O 3.4.1风力机特征风速的确定.......................................................................................... 29
" s3 L g/ x7 m& J7 z. z 3.4.2叶片重要参数选取..............................................................................................30
7 D. i s# L( ~( j7 w5 b 3.4.3叶展形状设计...................:..........................................................................323 H/ w3 ~8 N! M$ k9 s8 G @9 A
3.5设计结果形象化................................................................................................41
0 \1 O5 M/ R1 X9 C; C 3.5.1叶片截面空间坐标的求解...................................................................................... 413 ^( d( g/ n5 e1 \0 b
3.5.2叶片计算机3D绘图............................................................................................... 445 B Y8 _- I. t3 Y1 u
3.5.3该3D建模方法的优点........................................................................................... 45
. y7 X' L0 E! M, v/ G$ V5 @" U3.6叶片模型图......................................................................................................... 465 x4 [# h( M+ ]8 q+ g* k y
3.7本章小结................................................................................................................47, [& n9 @" ^1 H# g0 ?
第四章静态气动性能模拟计算........................:.............................. 484 E& R8 v( @) s `
4.1前言.......................................................................................................48$ b9 X& C- u i x6 c
4.1.1有量纲性能指标...................................................................................................... 48
) L( N" L( @" A/ {. {, `$ n% e7 M 4.1.2无量纲性能指标、..................................................................................................... 48: ^( ~- R0 N0 s+ P$ W7 L6 M! F
4.1.3有量纲指标和无量纲指标关系......................................................................486 p; q9 R3 g) B
4.2叶片气动性能计算...............................................................................................49% a3 r; Y: Y% N; ?8 t
4.2.1贝茨模型..........................................................................................................49; \# B5 b: H& B! O+ ^8 b
4.2.2涡流模型—Glauert模型和Wilson模型.................................................49" o8 ~5 r1 | y6 Q& _3 I
4.3各种修正系数..............................................................................................54
; P& o+ V9 g9 H5 Q+ ` 4.3.1叶片数修正...................................................................................54
& S& U6 s# o' Z 4.3.2翼型修正....................................................................................................55$ v' _1 X: \: l( [# h$ I& f: ~9 i, k
4.3.3叶尖修正..........................................................................................................553 [6 U, X7 J6 G0 R
4.3.4轮毅修正..............................................................................................................56& c$ ^9 k: D9 C. P' G/ g1 M/ y4 t
4.4模型修正结果................................................................................................56
* l7 x9 ?3 K) V" s' U9 r 4.4.1性能修正表..........................................................................................................57% b4 b9 [% E" ?- O1 S: D
4.4.2结果分析..........................................................................................................60
# @7 Z! w4 `" ^7 z$ K7 F4.5本章小结........................................................................................................................ 615 ?: O4 W. t# V% f; C; B- l, {
第五章叶片动力学分析........................................................... 62
* K" [0 t, T) f4 ?: \8 K: U- P广西大学祠盯士学位金仑.弋8 M3 f3 k8 N* u' E4 l" f: X+ P! `2 b& V
风办发电机叶少卜宝又计笼开乡t
/ Z# s/ k" L# \8 O% I6 c5.1前言............................................................................................................62$ n% R7 [+ H$ X) e: r% t+ X
5.2动力学分析方法............................................................................................................ 62) j% G# o" V5 _5 o, }
5.3计算模型................................................................................................................63! y) i5 _4 Y" d% |: |( s9 @0 [7 |, W
5.4分析工具................................................................................................................63
' T3 D7 E. v' D) K7 B$ ?5.5分析步骤.............................、.............................................................................65
5 K# m: m; E& h 5.5.1有限元建模.............................................................................................................. 65 H1 k7 ^" W+ |% C* B
5.5.2施加约束..........................................................................................................67
9 f2 X6 u5 F) T: |2 L# w6 U5.6计算结果........................................................................................................67* m& ^5 F$ D8 c; }
5.6.1模态计算结果..................................................................................................67
4 p0 F9 \3 Y2 I2 L S* n& e5 y5 M 5.6.2结果分析..............................................................................................................68& c; N: C4 b9 L8 F% X# |7 X5 Y o% }
5.6.3对比计算.................................................................................................................. 72
8 _1 v8 r ~% T 5.6.4计算模型的改进...................................................................................................... 74
5 n0 G/ j- T- s" D 5.6.5结论..................................................................................................................74
0 K2 Y/ h7 q8 l f0 ]5.7本章小结................................................................................................................74# |8 F3 g& Q. V. _" Q; F- T' ?
备第六章结论及展望................................................................................ 76
* ?7 |% J4 l7 n; O* A. m6.1结论....................................................................................................................76
, [4 t6 B, N8 i' d* Q2 o) p6.2论文堕待解决的问题.................................................................................................... 77
6 _/ j0 P: f# }4 `6.3展望..................................................................................................................776 M/ q* c5 k. G" Q
参考文献.......................................................................:..783 ?( }3 |% N) P
附录1翼型NACA4412数据.....................................................82
! W8 |! e3 A% Z0 c# w( d) H附录2翼型NACA4412气动性能表(RE=500000) ............................................................ 83
0 x0 \' z7 a+ n! y4 @% `% t0 w附录3翼型NACA4412气动性能图(RE=500000) ................................................. 84
1 S% g. t- j, P [; X' D3 P致谢.......................................................................................................... 85
% S X) Y( @) c) B8 d. m6 @6 i3 C攻读学位期间发表的学术论文目录................................................................................... 86 |
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