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- [1] AN INVISCID-VISCOUS INTERACTION METHOD TO PREDICT THE BLADE-TO-BLADE PERFORMANCE OF AXIAL COMPRESSORSAERONAUTICAL QUARTERLY, 1980, 31 (AUG): : 173 - 196CALVERT, WJHERBERT, MV
- [2] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATIONJOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1981, 103 (03): : 603 - 603DESHPANDE, RBHANSEN, ECSEROVY, GKSOCKOL, PM
- [3] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATIONJOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (01): : 28 - 34HANSEN, ECSEROVY, GKSOCKOL, PM
- [4] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATIONMECHANICAL ENGINEERING, 1979, 101 (06) : 98 - 98HANSEN, ECSEROVY, GKSOCKOL, PM
- [5] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATION.Journal of engineering for power, 1980, 102 (01): : 28 - 34Hansen, E.C.Serovy, G.K.Sockol, P.M.
- [6] Blade Design of Multistage Axial-Flow Compressors.Fortschritt-Berichte der VDI-Zeitschriften, Reihe 4: Bauingenieurwesen, 1980, (57 pt 7):Grahl, Klaus
- [7] Criteria of Selection of Blade Profiles and Their Radial Stacking in the Design of Axial Compressors.Termotecnica Milano, 1984, 38 (01): : 63 - 73Pittaluga, Ferruccio
- [8] PREDICTION OF STEADY INVISCID COMPRESSIBLE FLOW ON A BLADE-TO-BLADE SURFACE BY FINITE-ELEMENT METHODASTRONAUTICS & AERONAUTICS, 1978, 16 (11): : B45 - B45PRINCE, TC
- [9] INVISCID-VISCOUS INTERACTION ANALYSIS OF COMPRESSOR CASCADE PERFORMANCEJOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1991, 113 (04): : 538 - 552BARNETT, MHOBBS, DEEDWARDS, DE
- [10] CALCULATION METHOD FOR INCOMPRESSIBLE VISCOUS, BLADE-TO-BLADE FLOW THROUGH RADIAL TURBOMACHINES WITH LOG-SPIRAL BLADE SURFACESJOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1979, 101 (03): : 450 - 458BOSMAN, CCHAN, KCHATTON, AP