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J-GLOBAL ID：200902002022881153   Reference number：91A0933777

Computer-aided conceptual aircraft configuration development by an integrated optimization approach.

最適化手法による電算機利用の航空機概念形状設定法
Author (4)：
HABERLAND C

About HABERLAND C

(Technische Univ. Berlin, DEU)

About Technische Univ. Berlin, DEU

, 
FENSKE W

About FENSKE W

(Technische Univ. Berlin, DEU)

About Technische Univ. Berlin, DEU

, 
KRANZ O

About KRANZ O

(Technische Univ. Berlin, DEU)

About Technische Univ. Berlin, DEU

, 
STOER R

About STOER R

(Technische Univ. Berlin, DEU)

About Technische Univ. Berlin, DEU


Material：
Congress of the International Council of the Aeronautical Sciences  (ICAS Proceedings)

About Congress of the International Council of the Aeronautical Sciences


Volume： 17th  Issue： 2  Page： 2164-2173  Publication year： 1990 
JST Material Number： C0995A  Document type： Proceedings
Article type： 原著論文  Country of issue： Other (ZZZ)  Language： ENGLISH (EN)
Thesaurus term：
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optimization method

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,...
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Flying object design and structure 
(QK04010H)

About Flying object design and structure

Terms in the title (4)：
Terms in the title
Keywords automatically extracted from the title.
最適化手法

About 最適化手法

, 
電算機

About 電算機

, 
航空機

About 航空機

, 
概念

About 概念


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