Author: Leigh Ann Smith
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 48
Book Description
A Method for the Design of Transonic Flexible Wings
Author: Leigh Ann Smith
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 48
Book Description
A Method for the Design of Transonic Flexible Wings
Author: National Aeronautics and Space Adm Nasa
Publisher:
ISBN: 9781729363782
Category :
Languages : en
Pages : 48
Book Description
Methodology was developed for designing airfoils and wings at transonic speeds which includes a technique that can account for static aeroelastic deflections. This procedure is capable of designing either supercritical or more conventional airfoil sections. Methods for including viscous effects are also illustrated and are shown to give accurate results. The methodology developed is an interactive system containing three major parts. A design module was developed which modifies airfoil sections to achieve a desired pressure distribution. This design module works in conjunction with an aerodynamic analysis module, which for this study is a small perturbation transonic flow code. Additionally, an aeroelastic module is included which determines the wing deformation due to the calculated aerodynamic loads. Because of the modular nature of the method, it can be easily coupled with any aerodynamic analysis code. Smith, Leigh Ann and Campbell, Richard L. Langley Research Center RTOP 505-61-21-03...
Publisher:
ISBN: 9781729363782
Category :
Languages : en
Pages : 48
Book Description
Methodology was developed for designing airfoils and wings at transonic speeds which includes a technique that can account for static aeroelastic deflections. This procedure is capable of designing either supercritical or more conventional airfoil sections. Methods for including viscous effects are also illustrated and are shown to give accurate results. The methodology developed is an interactive system containing three major parts. A design module was developed which modifies airfoil sections to achieve a desired pressure distribution. This design module works in conjunction with an aerodynamic analysis module, which for this study is a small perturbation transonic flow code. Additionally, an aeroelastic module is included which determines the wing deformation due to the calculated aerodynamic loads. Because of the modular nature of the method, it can be easily coupled with any aerodynamic analysis code. Smith, Leigh Ann and Campbell, Richard L. Langley Research Center RTOP 505-61-21-03...
Applications of a Direct/iterative Design Method to Complex Transonic Configurations
Author: Leigh Ann Smith
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Scientific and Technical Aerospace Reports
NASA Technical Paper
NASA Scientific and Technical Publications: A Catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, 1991-1992
NASA Scientific and Technical Publications
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 400
Book Description
An Approach to Constrained Aerodynamic Design with Application to Airfoils
Author: Richard Lawson Campbell
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 28
Book Description
Inverse Problems in Engineering
Author: Keith A. Woodbury
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 532
Book Description
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 532
Book Description