Shock Waves @ Marseille I: Hypersonics, Shock Tube & Shock Tunnel Flow

ISBN-13: 9783642788314 / Angielski / Miękka / 2011 / 485 str.

Raymond Brun; Lucien Z. Dumitrescu

Opis

Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.

Spis treści

— Volume I.- Survey Paper.- Volume I: Hypersonics, Shock Tube and Shock Tunnel Flow — An Introductory Survey.- Plenary Lectures.- A Life with Shock Waves (Ernst Mach Memorial Lecture).- Computational Analysis on Generic Forms in European Hypersonic Facilities: Standard Model Electre and Hyperboloid-Flare.- Shock Tube Investigations of Combustion Phenomena in Supersonic Flows.- 1: Hypersonic Flow and Aerospace Studies.- Interference and Transient Effects on Compression Ramp Flows at Hypersonic Mach Numbers 41.- Effects of Leading-Edge Bluntness on Control Flap Effectiveness at Hypersonic Speeds.- Measuring the Effect of Nose Bluntness on Drag of a Cone in a Hypervelocity Shock Tunnel Facility.- Navier-Stokes Simulation and Measurement of Cone Drag at M? = 7.9.- The Boundary Layer on a Sharp Cone in High-Enthalpy Flow.- Shock Wave Interactions in Hypervelocity Flow.- Experimental Investigation of Shock-on-Shock Interactions in the High-Enthalpy Shock Tunnel Göttingen (HEG).- Oblique Shock Interactions with Mach Number Distributions.- Shock Wave/Boundary Layer Interaction in High-Enthalpy Compression Corner Flow.- Strength of Characteristics at a Curved Shock Wave.- Blunt Body Flow — The Transonic Region.- Shock Tube Application to the Study of Compressible Turbulent Boundary Layer With Mass Injection.- Interaction of Thermal Protection Materials with the High-Enthalpy Flow of the Arc-Heated Wind Tunnel LBK.- An Attractor-Driven Approximation for Turbulent Burst Dynamics in a Supersonic Free Shear Layer.- Effect of Nozzle Configurations on Unsymmetrical Supersonic Flows.- Radiative Heat Transfer from a Shock Layer Generated Around a Projectile Launched in a Ballistic Range.- Aerodynamic Heating in Three-Dimensional Bow Shock Wave/Turbulent Boundary Layer Interaction Region.- Parabolic Viscous Shock Layer Theory for 3D Hypersonic Gas Flow.- Viscous Hypersonic Flow over a Body Flying Through a Thermal in the Atmosphere.- 2: Combustion and Ram Accelerators.- Hydrogen Mixing and Combustion in a High-Enthalpy Hypersonic Stream.- Transverse Jet Mixing and Combustion Experiments in the Hypersonic Shock Tunnel T5 at GALCIT.- Three-Dimensional Mixing Flow Field in Supersonic Flow Induced by Injected Secondary Flow Through a Traverse Circular Nozzle.- Limitations of the Ram Accelerator.- Stability Studies of Detonation Driven Projectiles.- Bow Shock Wave Heating and Ablation of a Sharp-Nosed Projectile Flying Inside a Ram Accelerator.- In-Tube Photography of Ram Accelerator Projectiles.- 3: Shock Tube Technology and Diagnostic Techniques.- Hypervelocity Aerodynamics in a Superorbital Expansion Tube.- Influence of Secondary Diaphragm on Flow Quality in Expansion Tubes.- Noise Reduction in Argon Driven Expansion Tubes.- On the Principle, Design, and Performance of an Expansion-Shock Tube for Nucleation Studies.- High-Frequency Generation of High-Pressure Pulses Using a Diaphragmless Shock Tube.- A New Diaphragmless Shock Tube Facility for Interface Instability and Mach Reflection Studies.- Analysis of Calibration Results in the High-Enthalpy F4 Hot-Shot Wind Tunnel.- The Taylored Nozzle: A Method for Reducing the Convective Heat Transfer to Nozzle Throats by Gasdynamic Shielding.- Dealing with Pressure Oscillations in Stalker Tubes.- Comparison of the Flow in the High-Enthalpy Shock Tunnel in Göttingen with Numerical Simulations.- A Numerical and Experimental Study of the Free Piston Shock Tunnel.- Use of Argon-Helium Driver-Gas Mixtures in the T4 Shock Tunnel.- A Velocity Interferometric Study of the Performance of a Gas Gun.- Balances for the Measurement of Multiple Components of Force in Flows of a Millisecond Duration.- Further Developments of the ISL Millisecond Aerodynamic Force Measurement Technique.- Six-Component Force Measurement in the Aachen Shock Tunnel.- Driver Gas Detection by Quadrupole Mass Spectrometry in Shock Tunnels.- Skin Friction Measurements and Reynolds Analogy in a Hypersonic Boundary Layer.- Optical Studies of the Flow Start-up in Convergent-Divergent Nozzles.- Two Electric Discharge Methods for Visualizing Three-Dimensional Shock Shapes Around Hypersonic Vehicles.- Dual-Laser PLIF Imaging Techniques for Shock Tube Studies of Mixing and Combustion.- An Examination of the Aachen Shock Tunnel TH2 Gas Flows Using the HEG PLIF Apparatus.- 4: Numerical Computations.- Comparison of Numerical Methods 1: DSMC Simulations and N-S Predictions on Bluff Bodies.- Application of Multiblock Codes for Computational Aerothermodynamics of Hypersonic Vehicles.- Numerical Analysis of Shock/Shock and Shock/Body Interactions for 3D Configurations.- Hypersonic Shock-Wave/Boundary Layer Interactions with an Implicit Navier-Stokes Solver.- Visualisation of Shock Waves in Hypersonic CFD Solutions.- Shock Wave Interactions in Hypersonic Flow.- Numerical Simulation of Transient Bluff Body Flows.- An Efficient Unstructured Euler Solver for Transient Shocked Flows.- CTH: A Software Family for Multi-Dimensional Shock Physics Analysis.- Computation of Viscous Shock/Shock Interactions with an Upwind LU Implicit Scheme.- Numerical Calculations in Support of Complex Shock Interactions.- Numerical Simulation of Shock Induced Unsteady Aerodynamic Heating with a Highly Dense Mesh System.- A Comparison Study of Two Finite-Element Schemes for Computation of Shock Waves.- Adaptive Mesh Refinement Computation of Compressible Flow.- Shock-Capturing Schemes with Entropy Corrections and Dynamically Adaptive Unstructured Meshes.- Computing Complex Shocked Flows Through the Euler Equations.- A Third-Order ENO Scheme on Unstructured Meshes. Application to Shock Wave Calculations.- Numerical Simulation of Compressible Viscous Flows.- Time-Dependent Simulation of Reflected-Shock/Boundary Layer Interaction in Shock Tubes.- Numerical Simulation of Viscous Flow in a Super-Orbital Expansion Tube.- Analysis of the Flow Perturbations in a Shock Tube Due to the Curvature of the Diaphragm.- One-Dimensional Simulation of Free-Piston Shock Tunnel/Expansion Tubes.- Author Index.

Blurb

The book is devoted to hypersonics, including experimental work in shock tunnel flows with emphasis on the influence of "real gas" effects on aerodynamic phenomena encountered in hypersonics and aerospace studies. Numerical methods used for the determination of hypersonic flowfields, including chemical effects, are presented and applied to steady and unsteady configurations. The book also contains recent progress in shock tube and shock tube tunnel technology, including free piston shock tunnels, diaphragmless shock tubes, various processes for improving shock tube performances and numerous diagnostic techniques used in millisecond facilities such as force, moment measurements and optical methods. Papers on mixing problems in supersonic combustion and applications to ram accelerators are also in this volume.
This volume is addressed to scientists working on "hot" hypersonics, aerospace engineers, shock tube designers, researchers using shock tubes and associated equipment, and CFD people trying to simulate complex reactive flowfields.