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Image
( a ) Cross-sectional view of the axisymmetric intake with an elliptical li...
Published Online: October 4, 2022
Fig. 1 ( a ) Cross-sectional view of the axisymmetric intake with an elliptical lip adapted from Ref. [ 38 ] showing the major dimensions of the intake in terms of the intake diameter ( D i ). The measurement of the vortex circulation was carried out at a height 0.083 D l above the ground plan... More
Image
Location of the total pressure probes ( ) and static pressure probes (●) at...
Published Online: October 4, 2022
Fig. 2 Location of the total pressure probes ( ) and static pressure probes (●) at the AIP, for the flow from right to left. Data probe locations reproduced from fifth PAW participant guide [ 38 ]. (Color version online.) More
Image
Location of the total pressure probes ( ) and static pressure probes (●) at...
Published Online: October 4, 2022
Fig. 2 Location of the total pressure probes ( ) and static pressure probes (●) at the AIP, for the flow from right to left. Data probe locations reproduced from fifth PAW participant guide [ 38 ]. (Color version online.) More
Image
Variation of ( a )       Γ    *       and ( b ) DC60 with       U    *     ...
Published Online: October 4, 2022
Fig. 3 Variation of ( a ) Γ * and ( b ) DC60 with U * for the 8 M mesh ( ) and 33 M mesh ( ). The experimental and CFD results from Zantopp et al. (2010) [ 17 ] are shown by filled (●) and open symbols (◯), respectively. The black bars represent the dispersion of the ... More
Image
Variation of ( a )       Γ    *       and ( b ) DC60 with       U    *     ...
Published Online: October 4, 2022
Fig. 3 Variation of ( a ) Γ * and ( b ) DC60 with U * for the 8 M mesh ( ) and 33 M mesh ( ). The experimental and CFD results from Zantopp et al. (2010) [ 17 ] are shown by filled (●) and open symbols (◯), respectively. The black bars represent the dispersion of the ... More
Image
Variation of ( a )       Γ    *       and ( b ) DC60 with       U    *     ...
Published Online: October 4, 2022
Fig. 3 Variation of ( a ) Γ * and ( b ) DC60 with U * for the 8 M mesh ( ) and 33 M mesh ( ). The experimental and CFD results from Zantopp et al. (2010) [ 17 ] are shown by filled (●) and open symbols (◯), respectively. The black bars represent the dispersion of the ... More
Image
Variation of the ( a )       Γ    *       and ( b ) DC60 with     ψ     (°)...
Published Online: October 4, 2022
Fig. 4 Variation of the ( a ) Γ * and ( b ) DC60 with ψ (°) for the 33 million element mesh ( ) at U * = 19.8 . Results from simulations and experiments of Mishra et al. (2012) [ 19 ] are shown by filled (●) and open symbols (◯), respectively. (Color version ... More
Image
Variation of the ( a )       Γ    *       and ( b ) DC60 with     ψ     (°)...
Published Online: October 4, 2022
Fig. 4 Variation of the ( a ) Γ * and ( b ) DC60 with ψ (°) for the 33 million element mesh ( ) at U * = 19.8 . Results from simulations and experiments of Mishra et al. (2012) [ 19 ] are shown by filled (●) and open symbols (◯), respectively. (Color version ... More
Image
Isosurface plots of Q-criterion for ( a )     ψ  =   0      deg, ( b )     ...
Published Online: October 4, 2022
Fig. 5 Isosurface plots of Q-criterion for ( a ) ψ = 0  deg, ( b ) ψ = 15 deg, ( c ) ψ = 45 deg, and ( d ) ψ = 75 deg. The flow is directed into the page for the headwind cases, and as the yaw angle increase, the crosswind velocity approaches the intake from the ... More
Image
Visualization of the loss coefficient ( λ ) for the       U    *    =  6   ...
Published Online: October 4, 2022
Fig. 6 Visualization of the loss coefficient ( λ ) for the U * = 6 crosswind case for the 33 million element mesh. ( a ) Solution obtained from U * = 7.5 ( D C 60 = 0.084 ) and ( b ) solution obtained from a quiescent condition ( D C 60 = 0.066 ... More