E-raamat: Hypersonic Flows for Reentry Problems: Volume II: Test Cases - Experiments and Computations Proceedings of a Workshop Held in Antibes, France, 22-25 January 1990

Problems for Analysis.- Flow over a Slender Cone.- Problem 2: Turbulent
Base Flow.- Problem 3: Flow over a 2D Ramp.- Problem 4: Flow over a 3D
Obstacle.- Problem 5: Corner Flow.- Problem 6: Double (Simple) Ellipsoid.-
Problem 7: Flow over a Delta Wing.- Problem 8: Non-equilibrium Flow in an Arc
Jet or a Shock Tube.- Appendix: Non-equilibrium Model for Problem 6.-
Problems 1-2.- Hypersonic Boundary Layer and Base Flow.- Computation of
Hypersonic Turbulent Flow over a Rearward Facing Step.- Hypersonic Cone Flow
Predictions Using an Implicit Upwind Space-Marching Code.- Synthesis A
Synthesis of Results for Test Cases 1 and 2: Hypersonic Boundary Layer and
Base Flow.- Problems 3-4.- Experiments on Shock-Wave/Boundary-Layer
Interactions Produced by Two-Dimensional Ramps and Three-Dimensional
Obstacles.- An Experimental Contribution to the Flat Plate 2D Compression
Ramp, Shock/Boundary Layer Interaction Problem at Mach 14: Test Case 3.7.-
Viscous, 2-D, Laminar Hypersonic Flows over Compression Ramps.- Computational
Results for 2-D and 3-D Ramp Flows with an Upwind Navier-Stokes Solver.-
Application of the Galerkin/Least-Squares Formulation to the Analysis of
Hypersonic Flows: I. Flow over a Two-Dimensional Ramp.- The Application of an
Adaptive Upwind Unstructured Grid Solution Algorithm to the Simulation of
Compressible Laminar Viscous Flows over Compression Corners.- Computation of
Flows over 2D Ramps.- Hypersonic Viscous Flow over Two-Dimensional Ramps.-
Grid-Refinement Study of Hypersonic Laminar Flow over a 2-D Ramp.-
Contribution to Problem 3 Using a Galerkin Least Square Finite Element
Method.- Computational Results for Flows over Compression Ramps.- Implicit
Upwind Finite-Difference Simulation of Laminar Hypersonic Flow over a 2D
Ramp.- Synthesis A Synthesis of Results on the Calculation of Flow over a 2D
Ramp and a 3D Obstacle: Antibes Test Cases 3 and 4.- Problem 5.- Experimental
Study of the Longitudinal Hypersonic Corner Flow Field.- Problem 6.- 6.1
Non-reacting Flows.- Experimental Study of the Flow Around a Double Ellipsoid
Configuration.- Solution of the Euler Equations Around a Double Ellipsoidal
Shape Using Unstructured Meshes and Including Real Gas Effects.- Computation
of 2D Inviscid Hypersonic Flows Using Unstructured Polygonal Meshes.- An
Upwind Relaxation Method for Hypersonic Viscous Flows over a
Double-Ellipsoidal Body.- Navier-Stokes Calculations over a Double Ellipse
and a Double Ellipsoid by an Implicit Non-centered Method.- Application of
the Galerkin/Least-Squares Formulation to the Analysis of Hypersonic Flows:
II. Flow Past a Double Ellipse.- The Application of an Adaptive Unstructured
Grid Method to the Solution of Hypersonic Flows Past Double Ellipse and
Double Ellipsoid Configurations.- Computation of the Hypersonic Flow over a
Double Ellipsoid.- High Resolution Schemes for Steady Hypersonic Flow.-
Numerical Simulation of Laminar Hypersonic Flow Past a Double-Ellipsoid.-
Inviscid and Viscous Flow Calculation over a Double Ellipse with an Implicit
Centered Method.- 2D Hypersonic Viscous Flow Past a Double Ellipse Geometry.-
Hypersonic Flows over a Double or Simple Ellipse.- Solving Flow Equations for
High Mach Numbers on Overlapping Grids.- An Explicit Finite-Difference
Solution of Hypersonic Flows Using Rational Runge-Kutta Scheme.- Viscous and
Inviscid Hypersonic Flow About a Double Ellipsoid.- Numerical Simulation of
Hypersonic Flow over a Double Ellipse Using a Taylor-Galerkin Finite Element
Formulation with Adaptive Grids.- Hypersonic Viscous Flow Past Double Ellipse
and Past Double Ellipsoid - Numerical Results.- Adaptive Mesh Embedding for
Reentry Flow Problems.- Synthesis Attempt to Evaluate the Computation for
Test Case 6.1-Cold Hypersonic Flow Past Ellipsoidal Shapes.- 6.2/6.3 Reacting
Flows.- A Staggered Mesh Finite Difference Scheme for the Computation of
Hypersonic Euler Flows.- Reactive Flow Computations by Upwind Finite
Elements.- Numerical Analysis of Chemically Reacting Inviscid Flow in 2-D.- A
Contribution to the Prediction of Hypersonic Non-equilibrium Flows.- Reactive
and Inert Inviscid Flow Solutions by Quasi-linear Formulations and Shock
Fitting.- Inviscid Calculations by an Upwind Finite Element Method of
Hypersonic Flows over a Double (Single) Ellipse.- Contribution to Problem 6
Using an Upwind Euler Solver with Unstructured Meshes.- Inviscid Hypersonic
Flow Simulations Using an Explicit Scheme.- Computation of Thermochemical
Non-equilibrium Flows Around a Simple and a Double Ellipse.- Synthesis Some
Comments on the Numerical Computations of Reacting Flows over the
Double-Ellipse (Double Ellipsoid).- 6.4 Rarefied Flows.- DSMC Calculations
for the Double Ellipse.- Rarefied Flow Around a Double Ellipse.- The
Hypersonic Double Ellipse in Rarefied Flow.- Problem 7.- 7.1 Vortex Flows.-
Leeside Flow over Delta Wing at M = 7.15 Experimental Results for Test Case
7.1.2*.- Hypersonic Delta Wing Flow Calculations Using a Multidomain MUSCL
Euler Solver.- Finite Volume 3DNS and PNS Solutions of Hypersonic Viscous
Flow Around a Delta Wing Using Osher's Flux Difference Splitting.- Inviscid
Hypersonic Flow over a Delta Wing.- Hypersonic Leeside Delta-Wing-Flow
Computations Using Centered Schemes.- Synthesis Evaluation of Contributions
for Test Cases 7.1.1 and 7.1.2.- 7.2 Rarefied Flows.- Experimental Density
Flowfields over a Delta Wing Located in Rarefied Hypersonic Flows.-
Experiments on the Heat Transfer and on the Aerodynamic Coefficients of a
Delta Wing in Rarefied Hypersonic Flows.- DSMC Calculations for the Delta
Wing.- Rarefied Gas Flow Around a 3D-Deltawing.- Synthesis (Problems 6.4/7.2)
Appraisal of the Rarefied Flow Computations.- Problem 8.- Study of a Nitrogen
D.C. Plasma Torch at Different Pressures Using Optical and Thermal
Diagnostics.- Non-equilibrium Flow in an Arc-Jet.- Non-equilibrium Flow in an
Arc Heated Wind Tunnel.- Calculation of Non-equilibrium Flows in a
High-Enthalpy Wind Tunnel.- Application of Program LAURA to Thermochemical
Non-equilibrium Flow Through a Nozzle.- Non-equilibrium Flow in a Hypersonic
Wind Tunnel Nozzle.- Non-equilibrium Flow in a Hypersonic Wind Tunnel
Nozzle.- Quasi Monodimensional Inviscid Non-equilibrium Nozzle Flow
Computation.- Synthesis Non-equilibrium Flow in an Arcjet or a Shock Tube.-
Conclusion.- General Synthesis.- Index of Contributors.