Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing PDF Download

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Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing

Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing PDF Author: Joseph A. Yuska
Publisher:
ISBN:
Category : Aircraft
Languages : en
Pages : 108

Book Description
Test data are presented for a 38-cm (15-in.) diameter, 1.28 pressure ratio model VTOL lift fan installed in a two-dimensional wing and tested in a 2.74-by 4.58-meter (9-by 15-ft)V/STOL wind tunnel. Tests were run with and without exit louvers over a wide range of crossflow velocities and wing angle of attack. Tests were also performed with annular-inlet vanes, inlet bell-mouth surface disconuities, and fences to induce fan windmilling. Data are presented on the axial force of the fan assembly and overall wing forces and moments as measured on force balances for various static and crossflow test conditions. Midspan wing surface pressure coefficient data are also given.

Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing

Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing PDF Author: Joseph A. Yuska
Publisher:
ISBN:
Category : Aircraft
Languages : en
Pages : 108

Book Description
Test data are presented for a 38-cm (15-in.) diameter, 1.28 pressure ratio model VTOL lift fan installed in a two-dimensional wing and tested in a 2.74-by 4.58-meter (9-by 15-ft)V/STOL wind tunnel. Tests were run with and without exit louvers over a wide range of crossflow velocities and wing angle of attack. Tests were also performed with annular-inlet vanes, inlet bell-mouth surface disconuities, and fences to induce fan windmilling. Data are presented on the axial force of the fan assembly and overall wing forces and moments as measured on force balances for various static and crossflow test conditions. Midspan wing surface pressure coefficient data are also given.

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