Analytical Comparison of Hypersonic Flight and Wind Tunnel Viscous/inviscid Flow Fields
| Author | : H. J. Fivel |
| Publisher | : |
| Total Pages | : 130 |
| Release | : 1975 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
Analytical Comparison Of Hypersonic Flight And Wind Tunnel Viscous Inviscid Flow Fields
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Hypersonic Inviscid Flow
| Author | : Wallace D. Hayes |
| Publisher | : Courier Corporation |
| Total Pages | : 628 |
| Release | : 2012-07-13 |
| Genre | : Science |
| ISBN | : 0486160483 |
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.
Introduction to Hypersonic Flow
| Author | : Gorimir Gorimirovich Chernyĭ |
| Publisher | : |
| Total Pages | : 284 |
| Release | : 1961 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
Hypersonic Flow Theory
| Author | : Wallace Hayes |
| Publisher | : Elsevier |
| Total Pages | : 481 |
| Release | : 2012-12-02 |
| Genre | : Technology & Engineering |
| ISBN | : 032314876X |
Hypersonic Flow Theory presents the fundamentals of fluid mechanics, focusing on the hypersonic flow theory and approaches in theoretical aerodynamics. This book discusses the assumptions underlying hypersonic flow theory, unified supersonic-hypersonic similitude, two-dimensional and axisymmetric bodies, and circular cylinder. The constant-streamtube-area approximation, streamtube-continuity methods, and tangent-wedge and tangent-cone are also deliberated. This text likewise covers the similar laminar boundary layer solutions, bluntness induced interactions on slender bodies, and free molecule transfer theory. The dynamics of hypersonic flight or hypersonic wing theory, magnetohydrodynamic theory, or any developments involving treatment of the Boltzmann equation are not included. This publication is intended for hypersonic aerodynamicists, students, and researchers conducting work on the hypersonic flow phenomena.
Wind Tunnel Tests of Supersonic Two-dimensional and Half-axisymmetric Inlet Models in a Nonuniform Flow Field at Mach Numbers from 1.5 Through 2.5
| Author | : Frederick K. Hube |
| Publisher | : |
| Total Pages | : 274 |
| Release | : 1971 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Theoretical and Experimental Studies of Hypersonic Viscous Effects
| Author | : Clark Houston Lewis |
| Publisher | : |
| Total Pages | : 120 |
| Release | : 1965 |
| Genre | : Drag (Aerodynamics). |
| ISBN | : |
Analysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow
| Author | : John C. Adams |
| Publisher | : |
| Total Pages | : 98 |
| Release | : 1972 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Advances in Hypersonics: Computing hypersonic flows
| Author | : John J. Bertin |
| Publisher | : Birkhauser |
| Total Pages | : 0 |
| Release | : 1992 |
| Genre | : Science |
| ISBN | : 9780817636722 |
Approximate Two Layer (Inviscid/Viscous) Methods to Model Aerothermodynamic Environments.- Second-Order Effects in Hypersonic Boundary Layers.- Unstructured-Grid Algorithms for High-Speed CFD Analysis.- Numerical Simulation of Three-Dimensional Hypersonic Viscous Flows.- Numerical Simulation of Entry Flow over Blunt Swept-Wing Planes.- Viscous Nonequilibrium Flow Calculations.- The Finite Pointset Method for Hypersonic Flows in the Rarefied Gas Regime.- Computation of Flowfields for Hypersonic Flight at High Altitudes.
The High Temperature Aspects of Hypersonic Flow
| Author | : Wilbur C. Nelson |
| Publisher | : Elsevier |
| Total Pages | : 801 |
| Release | : 2014-12-02 |
| Genre | : Science |
| ISBN | : 1483223310 |
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
