JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
62275000.pdf2.4 MB
titleジェットエンジンサイクル検討における熱力学物性値について: その2
Other TitleThermodynamic properties of working substances on jet engine cycle studies: 2nd report
Author(jpn)二村, 尚夫
Author(eng)Futamura, Hisao
Author Affiliation(jpn)宇宙航空研究開発機構航空本部航空技術実証研究開発室(JAXA)
Author Affiliation(eng)Technology Demonstration Research Office, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)
Issue Date2014-03-31
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発資料
JAXA Research and Development Memorandum
VolumeJAXA-RM-13-019
Start page1
End page56
Publication date2014-03-31
Languagejpn
eng
Abstract前報に引き続き,ジェットエンジンにおける熱力学,内部空気力学に重要となる空気の熱力学物性値に関し,実在気体として取り扱う場合の基本的な状態方程式,データ数表を紹介する.
Thermodynamic properties of air is calculated accounted for real gas effect and compared with available data. Equations of state for pure substances and air are introduced and tabulated and drawn on charts for the thermodynamic functions.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Keywordsthermodynamics; real gas effect; standard atmosphere; themodynamic function; equation of state; virial coefficient; Helmholtz energy; phase transition; fugacity
Document TypeTechnical Report
JAXA Category研究開発資料
NASA Subject CategoryAircraft Propulsion and Power
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0062275000
Report NoJAXA-RM-13-019
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/20545


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