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Predicted tip flow loss in the rotor with BLI inlet distortion by physics-b...
Published Online: October 3, 2022
Fig. 4 Predicted tip flow loss in the rotor with BLI inlet distortion by physics-based loss models: ( a ) near choke condition, ( b ) peak efficiency condition, and ( c ) near stall condition More
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Comparison of loss prediction results and relative errors in cases under di...
Published Online: October 3, 2022
Fig. 10 Comparison of loss prediction results and relative errors in cases under different blade loads: ( a ) 90% rotating speed, ( b ) 95% rotating speed, ( c ) 100% rotating speed, and ( d ) 105% rotating speed More
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Distributions of test samples at different blade load conditions for the fu...
Published Online: October 3, 2022
Fig. 14 Distributions of test samples at different blade load conditions for the full-annulus fan rotor under BLI inflow distortion (Λ = 4.47%, 100% rotating speed) More
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Comparison of predicted loss and CFD results for each blade passage at diff...
Published Online: October 3, 2022
Fig. 15 Comparison of predicted loss and CFD results for each blade passage at different circumferential locations in the full-annulus fan rotor at different operating points (Λ = 4.47%, 100% rotating speed, ( a ) near choke point, ( b ) peak efficiency point, and ( c ) near stall point) More
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Comparisons of predicted loss and CFD results for different span fractions ...
Published Online: October 3, 2022
Fig. 16 Comparisons of predicted loss and CFD results for different span fractions at four typical circumferential locations in the full-annulus BLI fan (Λ = 4.47%, peak efficiency point, 100% rotating speed, ( a ) θ = 0 deg, ( b ) θ = 120 deg, ( c ) θ = 180 deg, and ( d ) θ = 240 deg) More
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Distributions of test samples at different rotating speeds for the full-ann...
Published Online: October 3, 2022
Fig. 17 Distributions of test samples at different rotating speeds for the full-annulus fan rotor under BLI inflow distortion (Λ = 4.47%, peak efficiency point) More
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Comparison of predicted loss and CFD results for each blade passage at diff...
Published Online: October 3, 2022
Fig. 18 Comparison of predicted loss and CFD results for each blade passage at different circumferential locations in the full-annulus fan rotor at different rotating speeds (Λ = 4.47%, peak efficiency point: ( a ) 95% rotating speed, ( b ) 100% rotating speed, and ( c ) 105% rotating speed) More
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Comparisons of predicted loss and CFD results for different span fractions ...
Published Online: October 3, 2022
Fig. 19 Comparisons of predicted loss and CFD results for different span fractions at four typical circumferential locations in the full-annulus BLI fan (Λ = 4.47%, peak efficiency point, 95% rotating speed: ( a ) θ = 0 deg, ( b ) θ = 120 deg, ( c ) θ = 180 deg, and ( d ) θ = 240 deg) More