Hypersonic Flows for Reentry Problems

Problems for Analysis.- Problem I: Flow over a Slender Cone.- Problem II: Turbulent Base Flow.- Problem EI: Flow over a 2D Ramp.- Problem IV: Flow over a 3D Obstacle.- Problem V: Corner Flow.- Problem VI: Double (Simple) Ellipsoid.- Problem VII: Flow over a Delta Wing.- Problem VIII: Non-equilibrium Flow in an Arc Jet or a Shock Tube.- Appendix I: Non-equilibrium Model for Problem VI.- Appendix II: Pitot Pressure and Mach Number Data at Station II, Problem II.- Summary: Comparison Workshop Part II (April 1991) and Part I (January 1990).- Inaugural Address.- Invited Lectures.- Hypersonic Research at German Universities — First Results of the Aachen Program.- Some Viscous Interactions Affecting the Design of Hypersonic Intakes and Nozzles.- Numerical Simulation of Scramjet Engine Flowfield.- Advances in Applied Mathematics Related to Hypersonic Flows.- Some Real Gas Shock Tunnel Experiments at Australian Universities.- Reacting Viscous Flow and Gas-Surface Interaction Modelling.- Problems I-II.- A Study of the Hypersonic Laminar/Turbulent Flow over a Slender Cone by the LCNS Code.- Computation of Hypersonic Flow over a Slender Cone.- Synthesis of Problems 1-2.- Problems III-IV.- 2D Laminar Ramp Flows.- Viscous Flow over a 2D Ramp.- Hypersonic Ramp Flow (Problem III. 1-4).- Computation of Hypersonic Flows over 2D Ramps with a Multigrid Method.- Computational Study of Laminar Hypersonic Flow over a 2D Ramp.- Hypersonic Viscous Flow Calculation over a 2D Ramp with an Implicit Centred Method Using No Artificial Viscosity.- Numerical Solution of the Navier-Stokes Equations for Hypersonic Ramps with the NS3GR Solver.- Contribution to Problem HI Using a Galerkin Least Squares Finite Element Method.- Flow over a 2D Ramp.- Implicit Upwind Finite-Difference Simulations of Laminar Hypersonic Flow over 2D Ramps.- Turbulent Compressible 2D and Axisymmetric Flows Computation with the K-Epsilon Model.- Navier-Stokes Computation over a 3D Ramp.- Computation of Hypersonic Flow Past a Compression Corner by a Spatial Marching Scheme.- A Finite Element Procedure for the Simulation of Viscous Compressible Flows.- Problem DI: 2D Ramp Flows.- Hypersonic Viscous Flow over a 2D Ramp.- Numerical Solution of Hypersonic Flows with Zonal Mesh Enrichment.- 2D Hypersonic Viscous Flow over Compression Ramps.- A Synthesis of Results for Problems III and IV: Flow over a 2D Ramp and a 3D Obstacle.- Problem V.- Hypersonic Corner Flow Detailed Experimental Study*.- Simulation of Laminar Hypersonic Flow About a Longitudinal Corner.- Laminar Navier-Stokes Calculations of the Flow in a Corner Geometry.- Synthesis for Problem V Longitudinal Hypersonic Corner Flow Field.- Problem VI.- Flow over Double Ellipsoid and Sphere - Experimental Results*.- Hypersonic Double-Ellipsoid Flow Cases VI. 1, VL5 and VL7.- Hypersonic Viscous Flow in Chemical Non-equilibrium.- Computation of Viscous Hypersonic Flows Using a Coupled Euler/Boundary Layer Method.- 2D and 3D Inviscid Hypersonic Flow Simulations Including Air Dissociation Effects.- Equilibrium Reactive Flow past the Double Ellipsoid at Mach = 25.- Computation of Flows Around a Double Ellipsoid.- Unstructured Grid Computations of Reactive Flows past Double Ellipse and Double Ellipsoid Configurations.- Non-equilibrium Double-Ellipse Flows by Adaptive Upwind Finite-Elements.- Problems VI. 1 and VI.8: Ellipsoid Euler-Bouridary Layer Calculation.- Special Aspects of Reacting Inviscid Blunt Body Flow.- 3D Inviscid Real Gas Flow over a Double-Ellipsoid.- Hypersonic Reacting Flow past Double Ellipse.- Numerical Solution of the Navier-Stokes Equations with Non-equilibrium Chemistry.- Synthesis of Problem VI: Double Ellipse/Ellipsoid and Sphere.- Problem VII.- Hypersonic Flow Field Computations Around a Double Ellipsoid and a Blunt Nosed Delta Wing.- Aerodynamic Forces Applied to a Delta Wing Located in Rarefied Hypersonic Flows*.- Force and Heat Transfer on a Delta Wing in Rarefied Flow*.- Pressure Measurements and Infrared Observation on the Windward Side of a Delta Wing*.- Hypersonic Delta Wing Flow Calculations Using a Multidomain MUSCL Euler Solver.- Euler Solution over a Hypersonic Blunt Nosed Delta Wing at High Angle of Attack.- Hypersonic Delta-Wing Flow, Problem VII.4.- Hypersonic Flow over a Delta Wing at High Angle of Attack.- Problem VII.4: Numerical Simulation of Laminar Hypersonic Flow over the Delta Wing.- Problem VII.4: Blunt Nose Delta Wing Euler Boundary Layer Calculation.- Flow over a Delta Wing.- DSMC Calculations for the Mini Delta Wing - Problem VH6.- Aerodynamic Performance of Delta Wings in the Hypersonic Rarefied Flow Regime. Comparison of 3D DSMC Simulation with Wind Tunnel Data.- DSMC Calculation on a Delta Wing — Problem VII.5.- Rarefied Gas Flow Around a 3D Delta Wing.- Delta Wing Flowfield Computations by Upwind and Centered TVD Techniques.- High Resolution Computation of 3D Inviscid Hypersonic Flows. Application to a Blunt Nose Delta Wing.- Synthesis of Problem VU: Delta Wing.- Synthesis of Problem VII: Rarefied Flow Test Cases.- Problem VIII.- Chemical and Vibrational Non-equilibrium Inviscid Hypersonic Nozzle Flows.- Numerical Simulation of Hypersonic Viscous and Reactive Flows in an Axisymmetric Nozzle.- Non-equilibrium Viscous Flows Calculations in a Hypersonic Nozzle.- Computation of a Non-equilibrium Flow with a Fully Coupled Implicit Solver.- Calculation of a Hypersonic Nozzle Flow.- A Contribution to the Analysis of High Enthalpy Nozzle Flows.- Numerical Solution of a Nozzle Flow.- Problem VIII 2: Non-equilibrium Flow in a Shock Tube.- Problem VIII. 1: Non-equilibrium Flow in an Arc Jet.- Non-equilibrium Flow in an Arc Jet.- Non-equilibrium Nitrogen Plasma Flow.- Non-equilibrium Flow in an Arcjet or a Shock Tube: Synthesis.- General Conclusion.- Index of Contributors.