Off-design correlation for losses due to part-span dampers on transonic rotors

[1]  D. C. Urasek,et al.  Performance of two-stage fan having low-aspect-ratio first-stage rotor blading , 1979 .

[2]  D. C. Urasek,et al.  Performance of two-stage fan with larger dampers on first-stage rotor , 1979 .

[3]  D. C. Urasek,et al.  Design and performance of a 427-meter-per-second-tip-speed two-stage fan having a 2.40 pressure ratio , 1978 .

[4]  R. S. Ruggeri,et al.  Performance with and without inlet radial distortion of a transonic fan stage designed for reduced loading in the tip region , 1978 .

[5]  W. B. Roberts Correlation of part-span damper losses through transonic rotors operating near design point , 1977 .

[6]  M. J. Keenan,et al.  Two-stage fan. 2: Data and performance with redesigned second stage rotor uniform and distorted inlet flows , 1974 .

[7]  W. M. Osborn,et al.  Performance of a single-stage transonic compressor with a blade-tip solidity of 1.5 and comparison with 1.3 and 1.7 solidity stages , 1973 .

[8]  D. C. Urasek,et al.  Performance of transonic fan stage with weight flow per unit annulus area of 198 kilograms per second per square meter (40.6(lb/sec)/sq ft) , 1973 .

[9]  G. Kovich,et al.  Overall and blade-element performance of a multiple-circular-arc bladed transonic compressor rotor with tip speed of 1375 feet per second , 1973 .

[10]  R. Moore,et al.  Performance of a single-stage axial-flow transonic compressor stage with a blade tip solidity of 1.7 , 1972 .

[11]  D. C. Urasek,et al.  Performance of a single-stage transonic compressor with a blade-tip solidity of 1.3 , 1972 .

[12]  D. C. Urasek,et al.  Comparison of the effect of two damper sizes on the performance of a low-solidity axial-flow transonic compressor rotor , 1972 .

[13]  V. L. Doyle,et al.  Evaluation of range and distortion tolerance for high Mach number transonic stages , 1970 .

[14]  Melvin J. Hartmann,et al.  A preliminary analysis of the magnitude of shock losses in transonic compressors , 1957 .

[15]  W. A. Benser,et al.  Holographic Studies of Shock Waves Within Transonic Fan Rotors , 1975 .

[16]  D. M. Sandercock,et al.  Some observed effects of part-span dampers on rotating blade row performance near design point , 1973 .