JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
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3
Other TitleThermodynamic properties of working substances on jet engine cycle studies: 3rd 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技術部門推進技術研究ユニット(JAXA)
Author Affiliation(eng)Propulsion Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)
Issue Date2017-03-31
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-16-010
Start page1
End page50
Publication date2017-03-31
Languagejpn
eng
Abstract前2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燃焼ガス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, データ数表等を紹介する.
Thermodynamic properties of combustion gas component molecules are calculated accounted for real gas effects and compared with available data with engineering review. Equations of state for pure substances and thermodynamic functions are tabulated and drawn on charts.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Keywordsthermodynamics; real gas effect; chemical equilibrium; combustion; thermodynamic function; equation of state; virial coefficient; Helmholtz free energy
Document TypeTechnical Report
JAXA Category研究開発資料
NASA Subject CategoryAircraft Propulsion and Power
ISSN1349-1121
NCIDAA11983593
SHI-NOAA1630054000
Report NoJAXA-RM-16-010
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/611130


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