共 13 条
- [1] Discussion: "The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascade" [ASME J. Turbomach., 122, No. 3, pp. 416-424 (2000)]JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 424 - 424Cumpsty, NA
- [2] The influence of technical surface roughness caused by precision forging on the flow around a highly loaded compressor cascadeJOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 416 - 424Leipold, RBoese, MFottner, L
- [3] Closure to "Discussion of 'Direction method for optimization of a centrifugal compressor vaneless diffuser' " (2001, ASME, J. Turbomach., 123, p. 79)JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (01): : 80 - 80Lee, YTLuo, LBein, TW
- [4] Closure to Discussion of ‘Measurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor’ (1993, ASME J. Turbomach., 115, p. 476)Journal of Turbomachinery, 1993, 115 (03): : 468 - 476Stauter, R.C.
- [5] Closure to Discussion of ‘On the Development and Application of the Fast-Response Aerodynamic Probe System for Turbomachines—Part 3: Comparison of Averaging Methods Applied to Centrifugal Compressor Measurements’ [ASME J. Turbomach., 122, No. 3, p. 527–535 (2000)]Journal of Turbomachinery, 2000, 122 (03):Kupferschmied, Peter
- [6] Closure to Discussion of ‘An Investigation of a Strong Shock-Wave Turbulent Boundary Layer Interaction in a Supersonic Compressor Cascade’ (1992, ASME J. Turbomach., 114, p. 503)Journal of Turbomachinery, 1992, 114 (03):Schreiber, H.A.Starken, H.
- [7] Closure to "Discussion of 'Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex' (2000-GT-506)" (2001, ASME J. Turbomach., 123, p. 461)JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (03): : 461 - 463Vogeler, KMailach, RLehmann, I
- [8] Closure to "Discussion of 'Development of advanced compressor airfoils for heavy-duty gas turbines - Part II: Experimental and theoretical analysis' " [ASME J. Turbomach., 122, No. 3, pp. 406-414 (2000)]JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 415 - 415不详
- [9] Closure to "Discussion of 'Comparative studies on short and long length-scale stall cell propagating in an axial compressor rotor' " (2001, ASME J. Turbomach., 123, p. 31)JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (01): : 31 - 32Inoue, MKuroumaru, MTanino, TYoshida, SFurukawa, M
- [10] Discussion: "Development of advanced compressor airfoils for heavy-duty gas turbines - Part II: Experimental and theoretical analysis" [ASME J. Turbomach., 122, No. 3, pp. 406-414 (2000)]JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2000, 122 (03): : 414 - 415Cumpsty, NA