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A direct and inverse boundary layer method for subsonic flow over delta wings

By Woodson, S. H.

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Book Id: WPLBN0002206784
Format Type: PDF eBook :
File Size: 0.8 MB
Reproduction Date: 2012
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Title: A direct and inverse boundary layer method for subsonic flow over delta wings  
Author: Woodson, S. H.
Volume:
Language: English
Subject: BOUNDARY VALUE PROBLEMS, INCOMPRESSIBLE FLOW, NUMERICAL ANALYSIS
Collections: NASA Publication Collection
Historic
Publication Date:
1986
Publisher:

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H, W. S., & R, D. F. (1986). A direct and inverse boundary layer method for subsonic flow over delta wings. Retrieved from http://medicallibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; A new inverse boundary layer method is developed and applied to incompressible flows with laminar separation and reattachment. Test cases fo

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: BOUNDARY VALUE PROBLEMS; INCOMPRESSIBLE FLOW; NUMERICAL ANALYSIS; COMPUTATIONAL FLUID DYNAMICS; NAVIER-STOKES EQUATION; PIPES (TUBES); SPECTRAL METHODS; TRANSONIC FLOW; VORTEX BREAKDOWN; COMPUTATIONAL GRIDS; FINITE ELEMENT METHOD; GAS DYNAMICS

 
 



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