Large-scale Wind-tunnel Investigation of a V/STOL Transport Model with Wing-mounted Lift Fans and Fuselage-mounted Life-cruise Engines for Propulsion PDF Download
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Author: Jerry V. Kirk
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 90
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Book Description
Author: Jerry V. Kirk
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 90
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Book Description
Author: Jerry V. Kirk
Publisher:
ISBN:
Category :
Languages : en
Pages : 86
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Author: William A. Newsom
Publisher:
ISBN:
Category : Downwash (Aerodynamics)
Languages : en
Pages : 110
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Book Description
Author: Joseph A. Yuska
Publisher:
ISBN:
Category : Aircraft
Languages : en
Pages : 108
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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.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 446
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Book Description
Author: William A. Newsom
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 134
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Book Description
Author: M. F. Platzer
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 548
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1346
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Book Description
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Book Description
