An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow: Computer program description 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 An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow: Computer program description PDF full book. Access full book title An Improved Method for the Aerodynamic Analysis of Wing-body-tail Configurations in Subsonic and Supersonic Flow: Computer program description by F. A. Woodward. Download full books in PDF and EPUB format.
Author: F. A. Woodward Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 324
Book Description
A new method has been developed for calculating the pressure distribution and aerodynamic characteristics of wing-body-tail combinations in subsonic and supersonic potential flow. A computer program has been developed to perform the numerical calculations. The configuration surface is subdivided into a large number of panels, each of which contains an aerodynamic singularity distribution. A constant source distribution is used on the body panels, and a vortex distribution having a linear variation in the streamwise direction is used on the wing and tail panels. The normal components of velocity induced at specified control points by each singularity distribution are calculated and make up the coefficients of a system of linear equations relating the strengths of the singularities to the magnitude of the normal velocities.
Author: F. A. Woodward Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 324
Book Description
A new method has been developed for calculating the pressure distribution and aerodynamic characteristics of wing-body-tail combinations in subsonic and supersonic potential flow. A computer program has been developed to perform the numerical calculations. The configuration surface is subdivided into a large number of panels, each of which contains an aerodynamic singularity distribution. A constant source distribution is used on the body panels, and a vortex distribution having a linear variation in the streamwise direction is used on the wing and tail panels. The normal components of velocity induced at specified control points by each singularity distribution are calculated and make up the coefficients of a system of linear equations relating the strengths of the singularities to the magnitude of the normal velocities.
Author: F. A. Woodward Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 140
Book Description
A new method has been developed for calculating the pressure distribution and aerodynamic characteristics of wing-body-tail combinations in subsonic and supersonic potential flow. A computer program has been developed to perform the numerical calculations. The configuration surface is subdivided into a large number of panels, each of which contains an aerodynamic singularity distribution. A constant source distribution is used on the body panels, and a vortex distribution having a linear variation in the streamwise direction is used on the wing and tail panels. The normal components of velocity induced at specified control points by each singularity distribution are calculated and make up the coefficients of a system of linear equations relating the strengths of the singularities to the magnitude of the normal velocities.
Author: F. A. Woodward
Author: F. A. Woodward
Author: F. A. Woodward
Author: 
Author: F.A. Woodward
Author: F.A. Woodward
Author: William Jackson Breedlove
Author: F.A. Woodward
Author: United States. National Aeronautics and Space Administration
Author: 
Author: