About: Oblique shock is a(n) research topic. Over the lifetime, 6551 publication(s) have been published within this topic receiving 119823 citation(s).
Papers published on a yearly basis
01 Feb 1986
TL;DR: In this article, Navier-Stokes et al. discuss the fundamental principles of Inviscid, Incompressible Flow over airfoils and their application in nonlinear Supersonic Flow.
Abstract: TABLE OF CONTENTS Preface to the Fifth Edition Part 1: Fundamental Principles 1. Aerodynamics: Some Introductory Thoughts 2. Aerodynamics: Some Fundamental Principles and Equations Part 2: Inviscid, Incompressible Flow 3. Fundamentals of Inviscid, Incompressible Flow 4. Incompressible Flow Over Airfoils 5. Incompressible Flow Over Finite Wings 6. Three-Dimensional Incompressible Flow Part 3: Inviscid, Compressible Flow 7. Compressible Flow: Some Preliminary Aspects 8. Normal Shock Waves and Related Topics 9. Oblique Shock and Expansion Waves 10. Compressible Flow Through Nozzles, Diffusers and Wind Tunnels 11. Subsonic Compressible Flow Over Airfoils: Linear Theory 12. Linearized Supersonic Flow 13. Introduction to Numerical Techniques for Nonlinear Supersonic Flow 14. Elements of Hypersonic Flow Part 4: Viscous Flow 15. Introduction to the Fundamental Principles and Equations of Viscous Flow 16. A Special Case: Couette Flow 17. Introduction to Boundary Layers 18. Laminar Boundary Layers 19. Turbulent Boundary Layers 20. Navier-Stokes Solutions: Some Examples Appendix A: Isentropic Flow Properties Appendix B: Normal Shock Properties Appendix C: Prandtl-Meyer Function and Mach Angle Appendix D: Standard Atmosphere Bibliography Index
01 Jan 1953
TL;DR: In this paper, the Hodograph Method for Two-Dimensional, Subsonic Flow with Small Perturbations is used to describe the dynamics of two-dimensional and three-dimensional flow.
Abstract: Partial table of contents: BACKGROUND. Foundations of Fluid Dynamics. Foundations of Thermodynamics. ONE--DIMENSIONAL FLOW. Isentropic Flow. Normal Shock Waves. Flow in Ducts with Heating or Cooling. INTRODUCTION TO FLOW IN TWO AND THREE DIMENSIONS. The Equations of Motion for Steady, Irrotational Flow. SUBSONIC FLOW. Hodograph Method for Two--Dimensional, Subsonic Flow. Three--Dimensional, Subsonic Flow. SUPERSONIC FLOW. Two--Dimensional, Supersonic Flow with Small Perturbations. Oblique Shocks. Appendices. Index.
03 Feb 2020
TL;DR: In this article, the conservation equation for Inviscid flows is revisited: Velocity Potential Equation, Linearized Flow, and Time-Marching Technique for Steady Supersonic Flow.
Abstract: 1 Compressible Flow - Some History and Introductory Thoughts 2 Integral Forms of the Conservation Equations for Inviscid Flows 3 One-Dimensional Flow 4 Oblique Shock and Expansion Waves 5 Quasi-One-Dimensional Flow 6 Differential Conservation Equations for Inviscid Flows 7 Unsteady Wave Motion 8 General Conservation Equations Revisited: Velocity Potential Equation 9 Linearized Flow 10 Conical Flow 11 Numerical Techniques for Steady Supersonic Flow 12 The Time-Marching Technique: With Application to Supersonic Blunt Bodies and Nozzles 13 Three-Dimensional Flow 14 Transonic Flow 15 Hypersonic Flow 16 Properties of High-Temperature Gases 17 High-Temperature Flows: Basic Examples Appendix A Appendix B An Illustration and Exercise of Computational Fluid Dynamics
01 Jan 1972-Fluid Dynamics
TL;DR: In this paper, an experimental study of the stability of the interface of two gases traversed by ash-wave was conducted and it was found that the interface is unstable both in the case of shock wave passage from the lighter to the heavier gas and for passage in the opposite direction.
Abstract: Results are presented of an experimental study of the stability of the interface of two gases traversed by ashockwave. It is found that the interface is unstable both in the case of shock wave passage from the lighter to the heavier gas and for passage in the opposite direction. The interface disturbance grows linearly with time in the first approximation.
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