Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1090
Book Description
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1090
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1090
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 910
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 910
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 306
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 306
Book Description
Flutter Studies to Determine Nacelle Aerodynamic Effects on a Fan-jet Transport Model for Two Mount Systems and Two Wind Tunnels
Author: Moses G. Farmer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transport airplane have been conducted primarily to determine the nacelle aerodynamic effects for high-bypass-ratio fan-jet engines. Data were obtained on a vertical rod mount in two wind tunnels and on a two-cable mount in one of the tunnels. The flutter response of the model was found to be dependent on nacelle aerodynamics, engine-pylon stiffness, mount-system-wind-tunnel configuration, and mass ratio.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transport airplane have been conducted primarily to determine the nacelle aerodynamic effects for high-bypass-ratio fan-jet engines. Data were obtained on a vertical rod mount in two wind tunnels and on a two-cable mount in one of the tunnels. The flutter response of the model was found to be dependent on nacelle aerodynamics, engine-pylon stiffness, mount-system-wind-tunnel configuration, and mass ratio.
Research Abstracts
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 418
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 418
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 32
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 606
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 606
Book Description
Nuclear Science Abstracts
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1308
Book Description
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1308
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 462
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 462
Book Description