LEADER 04527nam 22006013u 450 001 9911006632203321 005 20230801234117.0 010 $a1-5231-0964-5 010 $a0-486-16048-3 035 $a(CKB)3710000000317935 035 $a(EBL)1890418 035 $a(MiAaPQ)EBC1890418 035 $a(Au-PeEL)EBL1890418 035 $a(CaONFJC)MIL568230 035 $a(OCoLC)868966234 035 $a(EXLCZ)993710000000317935 100 $a20141222d2012|||| u|| | 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aHypersonic Inviscid Flow 205 $a1st ed. 210 $aNewburyport $cDover Publications$d2012 215 $a1 online resource (1074 p.) 225 1 $aDover Books on Physics 300 $aDescription based upon print version of record. 311 08$a0-486-43281-5 327 $aTitle 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 327 $a3. 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 327 $a6. 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 327 $a9. 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 327 $aMATHEMATICAL AND SPECIAL SYMBOLSAUTHOR INDEX 330 $a This treatment of the branch of fluid mechanics known as hypersonic inviscid flow offers a self-contained, unified view of nonequilibrium effects, body geometries, and similitudes available in hypersonic flow and thin shock layer theory. Seeking to cultivate readers' appreciation of theory, the text avoids empirical approaches and focuses on basic theory and related fundamental concepts.Contents include introductory materials and chapters on small-disturbance theory, Newtonian theory, constant-density solutions, the theory of thin shock layers, numerical methods for blunt-body flows, and oth 410 0$aDover Books on Physics 606 $aAerodynamics, Hypersonic 606 $aAir flow -- Mathematical models 606 $aInviscid flow 615 4$aAerodynamics, Hypersonic. 615 4$aAir flow -- Mathematical models. 615 4$aInviscid flow. 676 $a629.132 676 $a629.132306 700 $aHayes$b Wallace D$047618 701 $aProbstein$b Ronald F$021214 801 0$bAU-PeEL 801 1$bAU-PeEL 801 2$bAU-PeEL 906 $aBOOK 912 $a9911006632203321 996 $aHypersonic Inviscid Flow$94388605 997 $aUNINA