검색결과 : 5건
| No. | Article |
|---|---|
| 1 |
Inverse heat transfer method applied to capacitively cooled rocket thrust chambers Perakis N, Haidn OJ International Journal of Heat and Mass Transfer, 131, 150, 2019 |
| 2 |
Computing supersonic non-premixed turbulent combustion by an SMLD flamelet progress variable model Coclite A, Cutrone L, Gurtner M, De Palma P, Haidn OJ, Pascazio G International Journal of Hydrogen Energy, 41(1), 632, 2016 |
| 3 |
Improved combustion efficiency of a H-2/O-2 steam generator for spinning reserve application Haidn OJ, Frohlke K, Carl J, Weingartner S International Journal of Hydrogen Energy, 23(6), 491, 1998 |
| 4 |
P8 - The new French/German test facility for H-2/O-2 high pressure rocket engine combustion research Koschel WW, Haidn OJ International Journal of Hydrogen Energy, 23(8), 683, 1998 |
| 5 |
Spinning reserve system based on H-2/O-2 combustion Frohlke K, Haidn OJ Energy Conversion and Management, 38(10-13), 983, 1997 |