A Computational/Experimental Study of the Flow Around a Body of Revolution at Angle of Attack

A Computational/Experimental Study of the Flow Around a Body of Revolution at Angle of Attack
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
Total Pages: 34
Release: 2018-08-16
Genre:
ISBN: 9781725643284

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The incompressible Navier-Stokes equations are numerically solved for steady flow around an ogive-cylinder (fineness ration 4.5) at angle of attack. The three-dimensional vortical flow is investigated with emphasis on the tip and the near wake region. The implicit, finite-difference computation is performed on the CRAY X-MP computer using the method of pseudo-compressibility. Comparisons of computational results with results of a companion towing tank experiment are presented for two symmetric leeside flow cases of moderate angles of attack. The topology of the flow is discussed and conclusions are drawn concerning the growth and stability of the primary vortices. Zilliac, Gregory G. Ames Research Center NASA-TM-88329, A-86319, NAS 1.15:88329 RTOP 505-60-31...

NASA Tech Briefs

NASA Tech Briefs
Author:
Publisher:
Total Pages: 76
Release: 1992-05
Genre: Technology
ISBN:

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Government Reports Annual Index

Government Reports Annual Index
Author:
Publisher:
Total Pages: 1120
Release: 1990
Genre: Government reports announcements & index
ISBN:

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Hypersonic and High Temperature Gas Dynamics

Hypersonic and High Temperature Gas Dynamics
Author: John David Anderson
Publisher: AIAA
Total Pages: 710
Release: 1989
Genre: Science
ISBN: 9781563474590

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This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Aeronautical Engineering

Aeronautical Engineering
Author:
Publisher:
Total Pages: 538
Release: 1991
Genre: Aeronautics
ISBN:

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