語系:
繁體中文
English
說明(常見問題)
回圖書館首頁
手機版館藏查詢
登入
回首頁
切換:
標籤
|
MARC模式
|
ISBD
Simulation of thermoelastic behaviou...
~
Appel, Simon.
FindBook
Google Book
Amazon
博客來
Simulation of thermoelastic behaviour of spacecraft structures = fundamentals and recommendations /
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
Simulation of thermoelastic behaviour of spacecraft structures/ by Simon Appel, Jaap Wijker.
其他題名:
fundamentals and recommendations /
作者:
Appel, Simon.
其他作者:
Wijker, Jaap.
出版者:
Cham :Springer International Publishing : : 2022.,
面頁冊數:
xxiv, 399 p. :ill. (some col.), digital ;24 cm.
內容註:
Thermoelastic verification -- Occurrence of thermoelastic phenomenon in Spacecraft -- Physics of thermoelastics -- Modelling for thermoelastic -- Thermal modelling for thermo-elastic analysis -- Structural modelling for thermoelastic analysis -- Transfer of thermal analysis results to the structural model -- Prescribed Average Temperature Method -- Generation of linear conductors for lumped parameter thermal models -- Estimating uncertainties in the thermoelastic analysis process -- Solutions.
Contained By:
Springer Nature eBook
標題:
Space vehicles - Thermodynamics. -
電子資源:
https://doi.org/10.1007/978-3-030-78999-2
ISBN:
9783030789992
Simulation of thermoelastic behaviour of spacecraft structures = fundamentals and recommendations /
Appel, Simon.
Simulation of thermoelastic behaviour of spacecraft structures
fundamentals and recommendations /[electronic resource] :by Simon Appel, Jaap Wijker. - Cham :Springer International Publishing :2022. - xxiv, 399 p. :ill. (some col.), digital ;24 cm. - Springer aerospace technology,1869-1749. - Springer aerospace technology..
Thermoelastic verification -- Occurrence of thermoelastic phenomenon in Spacecraft -- Physics of thermoelastics -- Modelling for thermoelastic -- Thermal modelling for thermo-elastic analysis -- Structural modelling for thermoelastic analysis -- Transfer of thermal analysis results to the structural model -- Prescribed Average Temperature Method -- Generation of linear conductors for lumped parameter thermal models -- Estimating uncertainties in the thermoelastic analysis process -- Solutions.
This book provides recommendations for thermal and structural modelling of spacecraft structures for predicting thermoelastic responses. It touches upon the related aspects of the finite element and thermal lumped parameter method. A mix of theoretical and practical examples supports the modelling guidelines. Starting from the system needs of instruments of spacecraft, the reader is supported with the development of the practical requirements for the joint development of the thermal and structural models. It provides points of attention and suggestions to check the quality of the models. The temperature mapping problem, typical for spacecraft thermoelastic analysis, is addressed. The principles of various temperature mapping methods are presented. The prescribed average temperature method, co-developed by the authors, is discussed in detail together with its spin-off to provide high quality conductors for thermal models. The book concludes with the discussion of the application of uncertainty assessment methods. The thermoelastic analysis chain is computationally expensive. Therefore, the 2k+1 point estimate method of Rosenblueth is presented as an alternative for the Monte Carlo Simuation method, bringing stochastic uncertainty analysis in reach for large thermoelastic problems.
ISBN: 9783030789992
Standard No.: 10.1007/978-3-030-78999-2doiSubjects--Topical Terms:
3590084
Space vehicles
--Thermodynamics.
LC Class. No.: TL900 / .A66 2022
Dewey Class. No.: 629.471
Simulation of thermoelastic behaviour of spacecraft structures = fundamentals and recommendations /
LDR
:02916nmm a2200349 a 4500
001
2295892
003
DE-He213
005
20210831103933.0
006
m d
007
cr nn 008maaau
008
230324s2022 sz s 0 eng d
020
$a
9783030789992
$q
(electronic bk.)
020
$a
9783030789985
$q
(paper)
024
7
$a
10.1007/978-3-030-78999-2
$2
doi
035
$a
978-3-030-78999-2
040
$a
GP
$c
GP
041
0
$a
eng
050
4
$a
TL900
$b
.A66 2022
072
7
$a
TRP
$2
bicssc
072
7
$a
TEC002000
$2
bisacsh
072
7
$a
TRP
$2
thema
072
7
$a
TTDS
$2
thema
082
0 4
$a
629.471
$2
23
090
$a
TL900
$b
.A646 2022
100
1
$a
Appel, Simon.
$3
3590083
245
1 0
$a
Simulation of thermoelastic behaviour of spacecraft structures
$h
[electronic resource] :
$b
fundamentals and recommendations /
$c
by Simon Appel, Jaap Wijker.
260
$a
Cham :
$b
Springer International Publishing :
$b
Imprint: Springer,
$c
2022.
300
$a
xxiv, 399 p. :
$b
ill. (some col.), digital ;
$c
24 cm.
490
1
$a
Springer aerospace technology,
$x
1869-1749
505
0
$a
Thermoelastic verification -- Occurrence of thermoelastic phenomenon in Spacecraft -- Physics of thermoelastics -- Modelling for thermoelastic -- Thermal modelling for thermo-elastic analysis -- Structural modelling for thermoelastic analysis -- Transfer of thermal analysis results to the structural model -- Prescribed Average Temperature Method -- Generation of linear conductors for lumped parameter thermal models -- Estimating uncertainties in the thermoelastic analysis process -- Solutions.
520
$a
This book provides recommendations for thermal and structural modelling of spacecraft structures for predicting thermoelastic responses. It touches upon the related aspects of the finite element and thermal lumped parameter method. A mix of theoretical and practical examples supports the modelling guidelines. Starting from the system needs of instruments of spacecraft, the reader is supported with the development of the practical requirements for the joint development of the thermal and structural models. It provides points of attention and suggestions to check the quality of the models. The temperature mapping problem, typical for spacecraft thermoelastic analysis, is addressed. The principles of various temperature mapping methods are presented. The prescribed average temperature method, co-developed by the authors, is discussed in detail together with its spin-off to provide high quality conductors for thermal models. The book concludes with the discussion of the application of uncertainty assessment methods. The thermoelastic analysis chain is computationally expensive. Therefore, the 2k+1 point estimate method of Rosenblueth is presented as an alternative for the Monte Carlo Simuation method, bringing stochastic uncertainty analysis in reach for large thermoelastic problems.
650
0
$a
Space vehicles
$x
Thermodynamics.
$3
3590084
650
0
$a
Thermoelasticity.
$3
644512
650
1 4
$a
Aerospace Technology and Astronautics.
$3
928116
650
2 4
$a
Engineering Thermodynamics, Heat and Mass Transfer.
$3
1002079
650
2 4
$a
Solid Mechanics.
$3
3381524
650
2 4
$a
Astronomy, Astrophysics and Cosmology.
$3
890823
700
1
$a
Wijker, Jaap.
$3
3300951
710
2
$a
SpringerLink (Online service)
$3
836513
773
0
$t
Springer Nature eBook
830
0
$a
Springer aerospace technology.
$3
1566537
856
4 0
$u
https://doi.org/10.1007/978-3-030-78999-2
950
$a
Engineering (SpringerNature-11647)
筆 0 讀者評論
館藏地:
全部
電子資源
出版年:
卷號:
館藏
1 筆 • 頁數 1 •
1
條碼號
典藏地名稱
館藏流通類別
資料類型
索書號
使用類型
借閱狀態
預約狀態
備註欄
附件
W9437795
電子資源
11.線上閱覽_V
電子書
EB TL900 .A66 2022
一般使用(Normal)
在架
0
1 筆 • 頁數 1 •
1
多媒體
評論
新增評論
分享你的心得
Export
取書館
處理中
...
變更密碼
登入