Inviscid Supersonic and Hypersonic Flow Around an Elliptic Nose
Author: Richard Douglas Archer
Publisher:
Published: 1963
Total Pages: 304
ISBN-13:
DOWNLOAD EBOOK →Author: Richard Douglas Archer
Publisher:
Published: 1963
Total Pages: 304
ISBN-13:
DOWNLOAD EBOOK →Author: You-lan Zhu
Publisher: Springer Science & Business Media
Published: 2013-06-29
Total Pages: 606
ISBN-13: 3662067072
DOWNLOAD EBOOK →Since the appearance of computers, numerical methods for discontinuous solutions of quasi-linear hyperbolic systems of partial differential equations have been among the most important research subjects in numerical analysis. The authors have developed a new difference method (named the singularity-separating method) for quasi-linear hyperbolic systems of partial differential equations. Its most important feature is that it possesses a high accuracy even for problems with singularities such as schocks, contact discontinuities, rarefaction waves and detonations. Besides the thorough description of the method itself, its mathematical foundation (stability-convergence theory of difference schemes for initial-boundary-value hyperbolic problems) and its application to supersonic flow around bodies are discussed. Further, the method of lines and its application to blunt body problems and conical flow problems are described in detail. This book should soon be an important working basis for both graduate students and researchers in the field of partial differential equations as well as in mathematical physics.
Author: Wallace D. Hayes
Publisher: Courier Corporation
Published: 2012-07-13
Total Pages: 628
ISBN-13: 0486160483
DOWNLOAD EBOOK →Unified, self-contained view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer; appropriate for graduate-level courses in hypersonic flow theory. 1966 edition.
Author:
Publisher:
Published: 1991
Total Pages: 1460
ISBN-13:
DOWNLOAD EBOOK →Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: University of Minnesota
Publisher:
Published: 1956
Total Pages: 388
ISBN-13:
DOWNLOAD EBOOK →Author: W. C. Armstrong
Publisher:
Published: 1976
Total Pages: 98
ISBN-13:
DOWNLOAD EBOOK →The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.