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Three dimensional steady and unsteady asymmetric flow past wings of arbitrary planforms

By Kandil, O. A.

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Book Id: WPLBN0002204683
Format Type: PDF eBook :
File Size: 1.1 MB
Reproduction Date: 2012

Title: Three dimensional steady and unsteady asymmetric flow past wings of arbitrary planforms  
Author: Kandil, O. A.
Volume:
Language: English
Subject: AERONAUTICAL ENGINEERING, CYBERNETICS, AIRCRAFT
Collections: NASA Publication Collection
Historic
Publication Date:
1977
Publisher:

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A, K. O., H, N. A., & H, A. E. (1977). Three dimensional steady and unsteady asymmetric flow past wings of arbitrary planforms. Retrieved from http://www.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; The nonlinear discrete vortex method was extended to treat the problem of asymmetric flows past a wing with leading-edge separation, includi

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: AERONAUTICAL ENGINEERING; CYBERNETICS; AIRCRAFT; AEROSPACE ENGINEERING; NAVIGATION INSTRUMENTS; ROCKET PROPELLANTS; DESIGN; ROCKET ENGINES; ROCKET VEHICLES; U.S.S.R.; AUTOMATIC CONTROL; AVIONICS

 

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