|
|
|
|
|
|
|
Paul Vieille Lecture: Relaxation effects in hypervelocity flow: selected contributions from the T5 Lab |
|
|
3 | (8) |
|
|
|
CFD contributions to high-speed shock-related problems - examples today and new features tomorrow |
|
|
11 | (8) |
|
|
|
Explosive eruptions of volcanos: simulation, shock tube methods and multi-phase mathematical models |
|
|
19 | (8) |
|
|
|
Ignition delay time measurements at practical conditions using a shock tube |
|
|
27 | (8) |
|
|
|
Material processing and surface reaction studies in free piston driven shock tube |
|
|
35 | (8) |
|
|
|
|
|
|
|
Molecular dynamics of shock waves in dense fluids |
|
|
43 | (8) |
|
|
|
|
|
SBLI control for wings and inlets |
|
|
51 | (8) |
|
|
|
|
|
Shock pattern in the plume of rocket nozzles - needs for design consideration |
|
|
59 | (10) |
|
|
|
|
|
|
A quick estimate of explosion-induced stress field in various media |
|
|
69 | (4) |
|
|
|
|
|
Attenuation properties of blast wave through porous layer |
|
|
73 | (6) |
|
|
|
|
|
|
|
|
|
Blast wave reflection from lightly destructible wall |
|
|
79 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Gram-range explosive blast scaling and associated materials response |
|
|
85 | (6) |
|
|
|
|
|
|
|
High-speed digital shadowgraphy of shock waves from explosions and gunshots |
|
|
91 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Modelling high explosives (HE) using smoothed particle hydrodynamics |
|
|
97 | (6) |
|
|
|
|
|
|
|
Modification of air blast loading transmission by foams and high density materials |
|
|
103 | (6) |
|
|
|
|
|
|
|
Multifunctional protective devices for localizing the blast impact when conducting the ground and underwater operations of explosion cutting |
|
|
109 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Propagation of the shock wave generated by two-dimensional beam focusing of a CO2 pulsed laser |
|
|
115 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Simulation of strong blast waves by simultaneous detonation of small charges - a conceptual study |
|
|
121 | (6) |
|
|
|
|
|
|
|
Small-scale installation for research of blast wave dynamics |
|
|
127 | (6) |
|
|
|
|
|
|
|
Strong blast in a heterogeneous medium |
|
|
133 | (8) |
|
|
|
Part III Chemically Reacting Flows |
|
|
|
Atomized fuel combustion in the reflected-shock region |
|
|
141 | (6) |
|
|
|
|
|
Coupling CFD and chemical kinetics: examples Fire II and Titan aerocapture |
|
|
147 | (6) |
|
|
|
|
|
|
|
Experimental investigation of catalytic and non-catalytic surface reactions on SiO2 thin films with shock heated oxygen gas |
|
|
153 | (6) |
|
|
|
|
|
|
|
|
|
Experimental investigation of interaction of strong shock heated oxygen gas on the surface of ZrO2 - a novel method to understand re-combination heating |
|
|
159 | (6) |
|
|
|
|
|
|
|
Further studies on initial stages in the shock initiated H2 - O2 reaction |
|
|
165 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Shock-tube development for high-pressure and low-temperature chemical kinetics experiments |
|
|
171 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Shock-tube study of tert-butyl methyl ether pyrolysis |
|
|
177 | (6) |
|
|
|
|
|
|
|
|
|
Temperature dependence of the soot yield in shock wave pyrolysis of carbon-containing precursors |
|
|
183 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Thermal reactions of o-dichlorobenzene. Single pulse shock tube investigation |
|
|
189 | (6) |
|
|
|
|
|
|
|
Wall heat transfer in shock tubes at long test times |
|
|
195 | (8) |
|
|
|
|
|
|
|
Part IV Detonation and Combustion |
|
|
|
A study on DDT processes in a narrow channel |
|
|
203 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Combustion in a horizontal channel partially filled with porous media |
|
|
209 | (6) |
|
|
|
|
|
Continuum/particle interlocked simulation of gas detonation |
|
|
215 | (6) |
|
|
|
|
|
Dependence of PDE performance on divergent nozzle and partial fuel filling |
|
|
221 | (6) |
|
|
|
|
|
|
|
Direct Monte-Carlo simulation of developing detonation in gas |
|
|
227 | (6) |
|
|
|
|
|
Effects of detailed chemical reaction model on detonation simulations |
|
|
233 | (6) |
|
|
|
|
|
|
|
|
|
Effects of flame jet configurations on detonation initiation |
|
|
239 | (6) |
|
|
|
|
|
|
|
|
|
Experimental and theoretical investigation of detonation of detonation and shock waves action on phase state of hydrocarbon mixture in porous media |
|
|
245 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Experimental and theoretical study of valveless fuel supply system for PDE |
|
|
251 | (6) |
|
|
|
|
|
|
|
|
|
Experimental investigation of ignition spark shock waves influence on detonation formation in hydroxygen mixtures |
|
|
257 | (6) |
|
|
|
|
|
|
|
|
|
Experimental study on the nonideal detonation for JB-9014 rate sticks |
|
|
263 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Experimental study on transmission of an overdriven detonation wave across a mixture |
|
|
269 | (6) |
|
|
|
|
|
|
|
|
|
Flow vorticity behavior in inhomogeneous supersonic flow past shock and detonation waves |
|
|
275 | (6) |
|
|
|
|
|
Ground reflection interaction with height-of-burst metalized explosions |
|
|
281 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
High-fidelity numerical study on the on-set condition of oblique detonation wave cell structures |
|
|
287 | (6) |
|
|
|
|
|
|
|
|
|
High-pressure shock tube experiments and modeling of n-dodecane/air ignition |
|
|
293 | (6) |
|
|
|
|
|
|
|
Implicit-explicit Runge-Kutta methods for stiff combustion problems |
|
|
299 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Near-field blast phenomenology of thermobaric explosions |
|
|
305 | (6) |
|
|
|
|
|
|
|
|
|
Numerical and theoretical analysis of the precursor shock wave formation at high-explosive channel detonation |
|
|
311 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Numerical study on shockwave structure of superdetonative ram accelerator |
|
|
317 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Numerical study on the self-organized regeneration of transverse waves in cylindrical detonation propagations |
|
|
323 | (6) |
|
|
|
|
|
On the mechanism of detonation initiations |
|
|
329 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Overview of the 2005 Northern Lights Trials |
|
|
335 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Physics of detonation wave propagation in 3D numerical simulations |
|
|
341 | (6) |
|
|
|
|
|
|
|
Propagation of cellular detonation in the plane channels with obstacles |
|
|
347 | (6) |
|
|
|
|
|
|
|
|
|
Re-initiation of detonation wave behind slit-plate |
|
|
353 | (6) |
|
|
|
|
|
|
|
|
|
Shock-to-detonation transition due to shock interaction with prechamber-jet cloud |
|
|
359 | (6) |
|
|
|
|
|
|
|
Shock-to-detonation transition in tube coils |
|
|
365 | (6) |
|
|
|
|
|
|
|
|
|
Simulation of hydrogen detonation following an accidental release in an enclosure |
|
|
371 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Spectroscopic studies of micro-explosions |
|
|
377 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Structural response to detonation loading in 90-degree bend |
|
|
383 | (6) |
|
|
|
|
|
|
|
Study on perforated plate induced deflagration waves in a smooth tube |
|
|
389 | (6) |
|
|
|
|
|
|
|
|
|
Unconfined aluminum particles-air detonation |
|
|
395 | (6) |
|
|
|
|
|
|
|
|
|
Viscous attenuation of a detonation wave propagating in a channel |
|
|
401 | (8) |
|
|
|
|
|
|
|
|
|
|
|
|
A diode laser absorption sensor for rapid measurements of temperature and water vapor in a shock tube |
|
|
409 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
A novel fast-response heat-flux sensor for measuring transition to turbulence in the boundary layer behind a moving shock wave |
|
|
415 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Application of HEG static pressure probe in HIEST |
|
|
421 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Application of laser-induced thermal acoustics to temperature measurement of the air behind shock waves |
|
|
427 | (6) |
|
|
|
Assessment of rotational and vibrational temperatures behind strong shock waves derived from Cars method |
|
|
433 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Availability of the imploding technique as an igniter for large-scale natural-gas-engines |
|
|
439 | (6) |
|
|
|
|
|
|
|
|
|
Experimental study of SiC-based ablation products in high-temperature plasma-jets |
|
|
445 | (6) |
|
|
|
|
|
On pressure measurements in blast wave flow fields generated by milligram charges |
|
|
451 | (6) |
|
|
|
|
|
|
|
|
|
Quantitative diagnostics of shock wave - boundary layer interaction by digital speckle photography |
|
|
457 | (8) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
A simulation technique for radiating shock tube flows |
|
|
465 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Aerodynamic force measurement technique with accelerometers in the impulsive facility HIEST |
|
|
471 | (6) |
|
|
|
|
|
|
|
|
|
On the free-piston shock tunnel at UniBwM (HELM) |
|
|
477 | (6) |
|
|
|
|
|
Progress towards a microfabricated shock tube |
|
|
483 | (8) |
|
|
|
|
|
Part VII Flow Visualisation |
|
|
|
A tool for the design of slit and cutoff in schlieren method |
|
|
491 | (6) |
|
|
|
|
|
|
|
Application of pressure-sensitive paints in high-speed flows |
|
|
497 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Doppler Picture Velocimetry (DPV) applied to hypersonics |
|
|
503 | (6) |
|
|
|
|
|
|
|
|
|
|
|
On the conservation laws for light rays across a shock wave: Toward computer design of an optical setup for flow visualization |
|
|
509 | (6) |
|
|
|
Shock stand-off distance over spheres flying at transonic speed ranges in air |
|
|
515 | (6) |
|
|
|
|
|
|
|
|
|
Shock tube study of the drag coefficient of a sphere |
|
|
521 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Three-dimensional interferometric CT measurement of discharging shock/vortex flow around a cylindrical solid body |
|
|
527 | (6) |
|
|
|
|
|
|
|
Vizualization of 3D non-stationary flow in shock tube using nanosecond volume discharge |
|
|
533 | (8) |
|
|
|
|
|
|
|
|
|
Part VIII Hypersonic Flow |
|
|
|
Assessment of the convective and radiative transfers to the surface of an orbiter entering a Mars-like atmosphere |
|
|
541 | (6) |
|
|
|
|
|
|
|
|
|
Base pressure and heat transfer on planetary entry type configurations |
|
|
547 | (6) |
|
|
|
|
|
|
|
|
|
Combustion performance of a scramjet engine with inlet injection |
|
|
553 | (6) |
|
|
|
|
|
|
|
|
|
Compare, a combined sensor system for re-entry missions |
|
|
559 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows |
|
|
565 | (6) |
|
|
|
|
|
|
|
Drag reduction by counterflow supersonic jet for a blunt cone in high enthalpy flows |
|
|
571 | (6) |
|
|
|
|
|
Effect of electric arc discharge on hypersonic blunt body drag |
|
|
577 | (6) |
|
|
|
|
|
Effect of the nose bluntness on the electromagnetic flow control for reentry vehicles |
|
|
583 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Enhanced design of a scramjet intake using two different RANS solvers |
|
|
589 | (6) |
|
|
|
|
|
Experimental and numerical investigation of film cooling in hypersonic flows |
|
|
595 | (6) |
|
|
|
|
|
Experimental and numerical investigation of jet injection in a wall bounded supersonic flow |
|
|
601 | (6) |
|
|
|
|
|
Experimental investigation of cowl shape and location on inlet characteristics at hypersonic Mach number |
|
|
607 | (6) |
|
|
|
|
|
Experimental investigation of heat transfer reduction using forward facing cavity for missile shaped bodies flying at hypersonic speed |
|
|
613 | (6) |
|
|
|
|
|
|
|
|
|
Extrapolation of a generic scramjet model to flight scale by experiments, flight data and CFD |
|
|
619 | (6) |
|
|
|
|
|
|
|
Force measurements of blunt cone models in the HIEST high enthalpy shock tunnel |
|
|
625 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
Investigations of separated flow over backward facing steps in IISc hypersonic shock tunnel |
|
|
631 | (6) |
|
|
|
|
|
|
|
Measurement of aerodynamic forces for missile shaped body in hypersonic shock tunnel using 6-component accelerometer based balance system |
|
|
637 | (6) |
|
|
|
|
|
|
|
Measurement of shock stand-off distance on a 120° blunt cone model at hypersonic Mach number in Argon |
|
|
643 | (4) |
|
|
|
|
|
Model for shock interaction with sharp area reduction |
|
|
647 | (6) |
|
|
|
|
|
Modelling dissociation in hypersonic blunt body and nozzle flows in thermochemical nonequilibrium |
|
|
653 | (6) |
|
|
|
|
|
Numerical and experimental investigation of viscous shock layer receptivity and instability |
|
|
659 | (6) |
|
|
|
|
|
|
|
|
|
Numerical rebuilding of the flow in a valve-controlled Ludwieg tube |
|
|
665 | (6) |
|
|
|
|
|
|
|
Numerical study of shock interactions in viscous, hypersonic flows over double-wedge geometries |
|
|
671 | (6) |
|
|
|
|
|
|
|
Numerical study of thermochemical relaxation phenomena in high-temperature nonequilibrium flows |
|
|
677 | (6) |
|
|
|
|
|
|
|
Numerical study of wall temperature and entropy layer effects on transitional double wedge shock wave/boundary layer interactions |
|
|
683 | (6) |
|
|
|
|
|
Similarity laws of re-entry aerodynamics - analysis of reverse flow shock and wake flow thermal inversion phenomena |
|
|
689 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Simultanous measurements of 2-D total radiation and Cars data from hypervelocity flow behind strong shock waves |
|
|
695 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Shock tunnel testing of a Mach 6 hypersonic waverider |
|
|
701 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Supersonic flow over axisymmetric cavities |
|
|
707 | (6) |
|
|
|
|
|
Tandem spheres in hypersonic flow |
|
|
713 | (6) |
|
|
|
|
|
|
|
Three dimensional experimental investigation of a hypersonic double-ramp flow |
|
|
719 | (6) |
|
|
|
|
|
|
|
|
|
Triple point shear layers in hypervelocity flow |
|
|
725 | (8) |
|
|
|
|
|
|
|
|
|
|
Auto-ignition of hydrogen-air mixture at elevated pressures |
|
|
733 | (6) |
|
|
|
|
|
|
|
|
|
Discrepancies between shock tube and rapid compression machine ignition at low temperatures and high pressures |
|
|
739 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ignition delay studies on hydrocarbon fuel with and without additives |
|
|
745 | (6) |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Ignition of hydrocarbon---containing mixtures by nanosecond discharge: experiment and numerical modelling |
|
|
751 | (6) |
|
|
|
|
|
|
|
|
|
|
|
Laser-based ignition of hydrogen-oxygen mixture |
|
|
757 | (6) |
|
|
|
|
|
|
|
Measurements of ignition delay times and OH species concentrations in DME/O2/Ar mixtures |
|
|
763 | (6) |
|
|
|
|
|
|
|
Shock tube study of artificial ignition of N2O:O2:H2:Ar mixtures |
|
|
769 | (6) |
|
|
|
|
|
|
|
Shock tube study of kerosene ignition delay |
|
|
775 | (6) |
|
|
|
|
|
|
|
|
|
Shock-tube study of the ignition delay time of tetraethoxysilane (TEOS) |
|
|
781 | (6) |
|
|
|
|
|
|
|
|
| Author Index |
|
787 | (8) |
| Keyword Index |
|
795 | |
