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IUTAM Symposium on Combustion in Supersonic Flows
Proceedings of the IUTAM Symposium held in Poitiers, France, 2–6 October 1995
herausgegeben von M. Champion und B. DeshaiesInhaltsverzeichnis
- Opening Lecture.
- Observations concerning supersonic combustion.
- I. Premixed and unpremixed combustion in supersonic flows.
- Invited Lecture: Some generic problems related to combustion of hydrogen and air in supersonic flows.
- Development of a three-dimensional code to investigate supersonic-combustion problems.
- Influence of turbulent fluctuations on the induction period of hydrogen-air combustion reaction.
- Shock induced combustion over a rectangular ramp.
- Optical measurements of hydrogen mixing in supersonic airflows.
- A new L. E. S. approach to simulate Cheng’s experiment.
- Flame-holding behind a wedge by incident shock waves.
- Effects of laminar flamelet structures on supersonic turbulent combustion.
- Numerical study of auto-ignation and combustion in supersonic hydrogen-air mixing layer.
- Experiments on the flame-holding mechanism of a newly devised strut in supersonic airflows.
- II. Practical systems: Scramjets.
- Scramjet engine tests at Mach 4 and 6.
- An industrial point of view on scramjet combustor design.
- Shock tube investigations of H2 combustion in a high temperature supersonic air flow (Scramjet).
- III. Heterogeneous Combustion.
- Detonation of the gas mixtures with inert solid particles.
- Catalytic combustion in a cold supersonic flow of hydrogen-air premixture.
- IV. Practical systems: Ramaccelerators and PDWA.
- Invited Lecture: Pulsed detonation engines: Key issues.
- Invited Lecture: The ram accelerator: Perspectives and experimental results already achieved.
- Numerical simulations of unstart phenomenon in Ramac device.
- The effects of two-phase combustion in Ram Accelerator.
- The-30 mm-caliber Scram Accelerator Ramac 30 of ISL.
- Expansion tube experiments for the investigation of ram-accelerator-related phenomena.
- The PDWA concept for hypersonicpropulsion.
- V. Fluid-dynamic aspects of supersonic combustion.
- Mixing enhancement by normal gas injection in supersonic mixing layer.
- Properties of energetic scales in a supersonic mixing layer.
- Numerical simulations of shock-turbulence interactions.
- LDV Investigation of turbulence phenomena in multiple shock wave / turbulent boundary layer interactions.
- VI. Applications of Detonation to Propulsion.
- Invited Lecture: Galloping detonations.
- Numerical simulations of a marginal detonation: Wave velocities and transverse wave structure.
- Direct initiation of gaseous detonation by interacting supersonic jets.
- Onset of oblique H2-air detonations enhanced by a turbulent jet.
- Dynamics of curved detonation front and critical conditions for detonation initiations.
- Initiation of detonation by mixing of supersonic acetylene and oxygen jets.