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Computer programs for calculating pressure distributions including vortex effects on supersonic monoplane or cruciform wing-body-tail combinations with round or elliptical bodies

By Dillenius, M. F. E.

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Book Id: WPLBN0002205617
Format Type: PDF eBook :
File Size: 22.4 MB
Reproduction Date: 2012

Title: Computer programs for calculating pressure distributions including vortex effects on supersonic monoplane or cruciform wing-body-tail combinations with round or elliptical bodies  
Author: Dillenius, M. F. E.
Volume:
Language: English
Subject: ATMOSPHERIC CIRCULATION, RECTANGLES, VORTICITY
Collections: NASA Publication Collection
Historic
Publication Date:
1979
Publisher:

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F. E, D. M., & N, N. J. (1979). Computer programs for calculating pressure distributions including vortex effects on supersonic monoplane or cruciform wing-body-tail combinations with round or elliptical bodies. Retrieved from http://community.worldlibrary.net/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; Computer programs are presented which are capable of calculating detailed aerodynamic loadings and pressure distributions acting on pitched

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: ATMOSPHERIC CIRCULATION; RECTANGLES; VORTICITY; TURBULENT FLOW; FLOW DISTRIBUTION; NUMERICAL FLOW VISUALIZATION; FLOW CHARACTERISTICS; KINETIC ENERGY; NUMERICAL ANALYSIS; POTENTIAL FLOW

 

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