The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence

The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence
Author :
Publisher :
Total Pages : 70
Release :
ISBN-10 : NASA:31769000455538
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence by : Benjamin R. Briggs

Download or read book The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence written by Benjamin R. Briggs and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:


The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence Related Books

The Numerical Calculation of Flow Past Conical Bodies Supporting Elliptic Conical Shock Waves at Finite Angles of Incidence
Language: en
Pages: 70
NASA Technical Note
Language: en
Pages: 412
Authors:
Categories:
Type: BOOK - Published: 1969 - Publisher:

DOWNLOAD EBOOK

Difference Methods for Initial-Boundary-Value Problems and Flow Around Bodies
Language: en
Pages: 606
Authors: You-lan Zhu
Categories: Mathematics
Type: BOOK - Published: 2013-06-29 - Publisher: Springer Science & Business Media

DOWNLOAD EBOOK

Since the appearance of computers, numerical methods for discontinuous solutions of quasi-linear hyperbolic systems of partial differential equations have been
Analytic Methods in Aircraft Aerodynamics
Language: en
Pages: 758
Authors:
Categories: Aerodynamics
Type: BOOK - Published: 1970 - Publisher:

DOWNLOAD EBOOK

Hypersonic Inviscid Flow
Language: en
Pages: 628
Authors: Wallace D. Hayes
Categories: Science
Type: BOOK - Published: 2012-07-13 - Publisher: Courier Corporation

DOWNLOAD EBOOK

Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for grad