Evaluation of Helicopter Noise Due to Blade-vortex Interaction for Five Tip Configurations 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 Evaluation of Helicopter Noise Due to Blade-vortex Interaction for Five Tip Configurations PDF full book. Access full book title Evaluation of Helicopter Noise Due to Blade-vortex Interaction for Five Tip Configurations by Danny R. Hoad. Download full books in PDF and EPUB format.
Author: Danny R. Hoad
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 84
Get Book Here
Book Description
Author: Danny R. Hoad
Publisher:
ISBN:
Category : Acoustical engineering
Languages : en
Pages : 84
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84
Get Book Here
Book Description
Author: Shyue-bin Chang
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 354
Get Book Here
Book Description
Author: Juan Abelló
Publisher:
ISBN:
Category :
Languages : en
Pages : 466
Get Book Here
Book Description
Author: Ruth McVoy Martin
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 32
Get Book Here
Book Description
Author: Wel-Chong Sim
Publisher:
ISBN:
Category :
Languages : en
Pages : 360
Get Book Here
Book Description
Author: Todd Darwin Ringler
Publisher:
ISBN:
Category :
Languages : en
Pages : 332
Get Book Here
Book Description
Author: Danny R. Hoad
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 112
Get Book Here
Book Description
Author: Henry E. Jones
Publisher:
ISBN:
Category : Unsteady flow (Aerodynamics)
Languages : en
Pages : 96
Get Book Here
Book Description
A study of the full-potential modeling of a blade-vortex interaction was made. A primary goal of this study was to investigate the effectiveness of the various methods of modeling the vortex. The model problem restricts the interaction to that of an infinite wing with an infinite line vortex moving parallel to its leading edge. This problem provides a convenient testing ground for the various methods of modeling the vortex while retaining the essential physics of the full three-dimensional interaction. A full-potential algorithm specifically tailored to solve the blade-vortex interaction (BVI) was developed to solve this problem. The basic algorithm was modified to include the effect of a vortex passing near the airfoil. Four different methods of modeling the vortex were used: (1) the angle-of-attack methods, (2) the lifting-surface method, (3) the branch-cut method, and (4) the split-potential method. A side-by-side comparison of the four models was conducted. these comparisons included comparing generated velocity fields, a subcritical interaction, and a critical interaction. The subcritical and critical interactions are compared with experimentally generate results. The split-potential model was used to make a survey of some of the more critical parameters which affect the BVI.
Author: Duck Joo Lee
Publisher:
ISBN:
Category : Helicopters
Languages : en
Pages : 190
Get Book Here
Book Description
