Numerical investigation of the PDRE performance with detailed chemistry

S. Sato, A. Matsuo, J. Kasahara, T. Endo

研究成果: Paper

2 引用 (Scopus)

抜粋

Performance analysis of the Pulse Detonation Rocket Engine (PDRE) is numerically conducted focusing on partially filled system. Initial explosives, inexplosive gas species, tube fill fraction, and equivalence ratio are chosen as parameters to clarify their effects on the performance of PDRE. The simulation results are compared with previous studies that used several explosives, and agreed well with them. The simulation results indicate that the initial mass fraction of explosive to the total mass is the dominant factor for the normalized Isp under arbitrary conditions. We newly propose the partial fill model to predict the performance of partially filled PDRE.

元の言語English
ページ943-951
ページ数9
出版物ステータスPublished - 2004 7 1
イベント42nd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States
継続期間: 2004 1 52004 1 8

Other

Other42nd AIAA Aerospace Sciences Meeting and Exhibit
United States
Reno, NV
期間04/1/504/1/8

    フィンガープリント

ASJC Scopus subject areas

  • Engineering(all)

これを引用

Sato, S., Matsuo, A., Kasahara, J., & Endo, T. (2004). Numerical investigation of the PDRE performance with detailed chemistry. 943-951. 論文発表場所 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, United States.