Author: Thomas P. Moffitt
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine
Author: Thomas P. Moffitt
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
Experimental Investigation of Partial and Full-admission Characteristics of a Two- Stage Velocity-compound Turbine
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Book Description
Scientific and Technical Aerospace Reports
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
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.
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.
NASA Technical Note
GAs Turbine Catalog
Turbine Design and Application
Author: Arthur J. Glassman
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 152
Book Description
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 436
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 436
Book Description