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規格・テクニカルリポート類

コンポジット固体ロケット推進薬のポアソン比測定

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コンポジット固体ロケット推進薬のポアソン比測定

Material type
規格・テクニカルリポート類
Author
大竹, 邦彦ほか
Publisher
航空宇宙技術研究所
Publication date
1973-08
Material Format
Digital
Capacity, size, etc.
-
NDC
-
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Notes on use

Note (General):

出版タイプ: NAPoisson's ratio is one of the most important factors that have the effect on the ac- curacy of the stress analysis of the solid propellant gr...

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
大竹, 邦彦
遠藤, 修司
種村, 利春
OOTAKE, Kunihiko
ENDO, Shuji
TANEMURA, Toshiharu
Publication, Distribution, etc.
Publication Date
1973-08
Publication Date (W3CDTF)
1973-08
Alternative Title
A Measurement of Poisson′s Ratio of CTPB Composite Solid Propellant
Periodical title
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
No. or year of volume/issue
245
Volume
245
Pages
12-
ISSN (Periodical Title)
ISSN : 0452-2982
Text Language Code
jpn
Target Audience
一般
Note (General)
出版タイプ: NA
Poisson's ratio is one of the most important factors that have the effect on the ac- curacy of the stress analysis of the solid propellant grain. It is often assumed, however, that the propellant is incompressible. Therefore Poisson's ratio takes the value of one half, especially at low strain levels. In the present investigation, Poisson's ratio is evaluated experimentally by the photographic method. In the experiment, a special care is paid for the size and the marking of the test specimens. The errors of the measurement by the photographic method may be mainly raised from the following two ; one depends on the projecting machine employed, and the other depeneds on the sharpness of the marks. The former is of inevitable nature. The latter is caused by the roughness of the propellant's surface, which is scarcely seen in rubber specimens. These errors can be canceled out by taking the average values. The experiment is conducted at the room temperature and at the strain rate of 0.03 mm/mm/min. The strains were calculated in accordance with the formula which defines the natural strains. Test results show that Poisson's ratio of the propellant has a value of 0.47+0.01 at the strain level up to 10%, and then the ratio decreases gradually because of the dewetting phenomena.
資料番号: NALTM0245000
レポート番号: NAL TM-245
Data Provider (Database)
国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
Original Data Provider (Database)
宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ