Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725610309
Category :
Languages : en
Pages : 34
Book Description
A method is developed that determines the placement of an active control surface for maximum effectiveness in suppressing flutter. No specific control law is required by this method which is based on the aerodynamic energy concept. It is argued that the spanwise placement of the active controls should coincide with the locations where maximum energy per unit span is fed into the system. The method enables one to determine the distribution, over the different surfaces of the aircraft, of the energy input into the system as a result of the unstable fluttering mode. The method is illustrated using three numerical examples. Nissim, E. and Burken, John J. Armstrong Flight Research Center NASA-TP-2873, H-1492, NAS 1.60:2873 RTOP 505-66-71...
Control Surface Spanwise Placement in Active Flutter Suppression Systems
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725610309
Category :
Languages : en
Pages : 34
Book Description
A method is developed that determines the placement of an active control surface for maximum effectiveness in suppressing flutter. No specific control law is required by this method which is based on the aerodynamic energy concept. It is argued that the spanwise placement of the active controls should coincide with the locations where maximum energy per unit span is fed into the system. The method enables one to determine the distribution, over the different surfaces of the aircraft, of the energy input into the system as a result of the unstable fluttering mode. The method is illustrated using three numerical examples. Nissim, E. and Burken, John J. Armstrong Flight Research Center NASA-TP-2873, H-1492, NAS 1.60:2873 RTOP 505-66-71...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725610309
Category :
Languages : en
Pages : 34
Book Description
A method is developed that determines the placement of an active control surface for maximum effectiveness in suppressing flutter. No specific control law is required by this method which is based on the aerodynamic energy concept. It is argued that the spanwise placement of the active controls should coincide with the locations where maximum energy per unit span is fed into the system. The method enables one to determine the distribution, over the different surfaces of the aircraft, of the energy input into the system as a result of the unstable fluttering mode. The method is illustrated using three numerical examples. Nissim, E. and Burken, John J. Armstrong Flight Research Center NASA-TP-2873, H-1492, NAS 1.60:2873 RTOP 505-66-71...
Control Surface Spanwise Placement in Active Flutter Suppression Systems
Author: E. Nissim
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Control Surface Spanwise Placement in Active Flutter Suppression Systems
Author: E. Nissim
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 24
Book Description
Control surface spanwise placement in active flutter suppresssion systems
Author: E. Nissim
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 16
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 312
Book Description
NASA Scientific and Technical Publications
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 92
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 882
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 882
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1480
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1480
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 24
Book Description
Control and Dynamic Systems V52: Integrated Technology Methods and Applications in Aerospace Systems Design
Author: C.T. Leonides
Publisher: Elsevier
ISBN: 032316319X
Category : Transportation
Languages : en
Pages : 563
Book Description
Control and Dynamic Systems: Advances in Theory and Applications, Volume 52: Integrated Technology Methods and Applications in Aerospace System Design discusses the various techniques and applications in aerospace systems. This book presents automation and integration techniques in optimizing aircraft structural design. It also covers a number of technologies used in aerospace systems such as active flutter suppression, flight control configuration, aeroassisted plane change missions, flight control systems, and impaired aircraft. This book concludes by demonstrating some modeling issues in command, control, and communication networks. This book is a significant reference source for engineers involved in aerospace systems design.
Publisher: Elsevier
ISBN: 032316319X
Category : Transportation
Languages : en
Pages : 563
Book Description
Control and Dynamic Systems: Advances in Theory and Applications, Volume 52: Integrated Technology Methods and Applications in Aerospace System Design discusses the various techniques and applications in aerospace systems. This book presents automation and integration techniques in optimizing aircraft structural design. It also covers a number of technologies used in aerospace systems such as active flutter suppression, flight control configuration, aeroassisted plane change missions, flight control systems, and impaired aircraft. This book concludes by demonstrating some modeling issues in command, control, and communication networks. This book is a significant reference source for engineers involved in aerospace systems design.