Hypersonic Inviscid Flow

• Autore: Hayes Wallace D
• Pubblicazione: Newburyport, : Dover Publications, 2012
• Edizione: 1st ed.
• Descrizione fisica: 1 online resource (1074 p.)
• Disciplina: 629.132; 629.132306
• Soggetto topico: Aerodynamics, Hypersonic; Air flow -- Mathematical models; Inviscid flow
• Altri autori: ProbsteinRonald F
• Note generali: Description based upon print version of record.
• Nota di contenuto: Title Page; Copyright Page; Dedication; PREFACE TO THE DOVER EDITION; PREFACE TO VOLUME I; PREFACE TO THE FIRST EDITION; Table of Contents; Erratum; CHAPTER I - GENERAL CONSIDERATIONS; 1. Introductory remarks; 2. General features of hypersonic flow fields; 3. Assumptions underlying inviscid hypersonic theory; 4. The normal shock wave; 5. Oblique and curved shocks; 6. Mach number independence principle; 7. General strip theory; 8. Dissipative effects; CHAPTER II - SMALL-DISTURBANCE THEORY; 1. Introduction and basic equations; 2. Hypersonic similitude ; 3. Unified supersonic-hypersonic similitude4. Slender-body strip theory; 5. Examples of small-disturbance solutions; 6. Similar power-law solutions; 7. Application of similar solutions to steady flows; 8. Slightly blunted slender bodies; 9. Large incidence and correlation of similitudes; 10. Unsteady flow theory; 11. Nonequilibrium effects; CHAPTER III - NEWTONIAN THEORY; 1. The gasdynamics of Sir Isaac Newton; 2. Two-dimensional and axisymmetric bodies; 3. Simple shapes and free layers; 4. Optimum shapes; 5. Shock layer structure and cross flow phenomena ; 6. Shock layer structure with cross flow7. Conical flow; 8. Bodies of revolution at small incidence; 9. Unsteady flow; CHAPTER IV - CONSTANT-DENSITY SOLUTIONS; 1. The wedge; 2. The cone; 3. Circular cylinder; 4. The sphere; 5. Solutions with cross flow; CHAPTER V - THE THEORY OF THIN SHOCK LAYERS; 1. Basic concepts; 2. Successive approximation schemes; 3. Constant-streamtube-area approximation; 4. Two-dimensional and axisymmetric blunt-faced bodies; 5. Quasi wedges and quasi cones; 6. Conical bodies; 7. General blunt-faced bodies and related similitudes; 8. Integral methods ; 9. Newtonian separation10. Nonequilibrium flows; CHAPTER VI - NUMERICAL METHODS FOR BLUNT-BODY FLOWS; 1. Nature of the problem; 2. Streamtube-continuity methods; 3. Method of integral relations and polynomial approximation; 4. Relaxation techniques and the unsteady approach method; 5. The inverse problem; 6. Procedures with nonequilibrium; CHAPTER VII - OTHER METHODS FOR LOCALLY SUPERSONIC FLOWS; 1. Method of characteristics; 2. Shock-expansion theory; 3. Tangent-wedge and tangent-cone; 4. Conical flows; 5. Nonequilibrium flows; CITED REFERENCES; SYMBOL INDEX; SUBSCRIPTS; SUPERSCRIPTS ; MATHEMATICAL AND SPECIAL SYMBOLSAUTHOR INDEX
• Sommario/riassunto: This treatment of the branch of fluid mechanics known as hypersonic inviscid flow offers a self-contained, unified view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer theory. Seeking to cultivate readers' appreciation of theory, the text avoids empirical approaches and focuses on basic theory and related fundamental concepts.Contents include introductory materials and chapters on small-disturbance theory, Newtonian theory, constant-density solutions, the theory of thin shock layers, numerical methods for blunt-body flows, and oth
• Titolo autorizzato: Hypersonic Inviscid Flow
• ISBN: 1-5231-0964-5; 0-486-16048-3
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9911006632203321
• Lo trovi qui: Univ. Federico II
• Serie: Dover Books on Physics