Subsonic Performance Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Subsonic Performance Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System PDF full book. Access full book title Subsonic Performance Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System by Francis J. Capone. Download full books in PDF and EPUB format.
Author: Francis J. Capone
Publisher:
ISBN:
Category : Lift fans
Languages : en
Pages : 282
Get Book Here
Book Description
Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers.
Author: Francis J. Capone
Publisher:
ISBN:
Category : Lift fans
Languages : en
Pages : 282
Get Book Here
Book Description
Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers.
Author: Brent K. Hodder
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 60
Get Book Here
Book Description
The low-speed aerodynamics of a large-scale triangular wing model, with a reduced thickness, tip-turbine driven lift fan in each wing were investigated in the Ames 40-by 80-Foot Wind Tunnel. The model had a 5-percent-thick wing typical of wings designed for supersonic performance. Conventional lift-fan depth has, in the past, limited wing thickness to about 10 percent. A thinner lift fan for the present investigation was obtained by modification of a conventional fan. The modification included removing the discharge stator and reducing the fan inlet length and radius. To control airflow separation resulting from small inlet radii, blowing boundary-layer control was applied through a nozzle in the inlet. Performance of the modified fan along with aerodynamic characteristics of the total configuration is presented. The static thrust performance of the conventional fan (requiring a lo-percent wing) was equalled by the reduced thickness fans of this investigation.--P. [i].
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 446
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 234
Get Book Here
Book Description
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 464
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970
Get Book Here
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Get Book Here
Book Description
