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- [2] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATION JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1981, 103 (03): : 603 - 603
- [3] AXIAL-FLOW COMPRESSOR TURNING ANGLE AND LOSS BY INVISCID-VISCOUS INTERACTION BLADE-TO-BLADE COMPUTATION JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (01): : 28 - 34
- [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 - 34
- [8] PREDICTION OF STEADY INVISCID COMPRESSIBLE FLOW ON A BLADE-TO-BLADE SURFACE BY FINITE-ELEMENT METHOD ASTRONAUTICS & AERONAUTICS, 1978, 16 (11): : B45 - B45
- [9] INVISCID-VISCOUS INTERACTION ANALYSIS OF COMPRESSOR CASCADE PERFORMANCE JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1991, 113 (04): : 538 - 552