Proceedings ArticleDOI
Supersonic Combustion - A Shock Tunnel and Vitiation-heated Slowdown Tunnel Comparison
TLDR
In this paper, a comparison between supersonic combustion in two commonly used, but fundamentally different, facilities for scramjet research - a vitiation-heated blowdown tunnel and a free piston shock tunnel -was made.Abstract:
A comparison has been made between supersonic combustion in two commonly used, but fundamentally different, facilities for scramjet research - a vitiation-heated blowdown tunnel and a free piston shock tunnel. By passing the shock tunnel freestream flow through a normal shock and then expanding it to Mach 2.5, combustor inlet conditions were nominally replicated between the two facilities, as were the combustor geometries. A straight rectangular duct and a diverging duct, both employing central strut hydrogen injection, were used. Boundary layer growth and separation in the straight duct limited meaningful comparisons to a fuel equivalence ratio Φ of the order of 0.20. With the diverging duct, comparisons were made up to Φ = 1.05. Reasonably good agreement between the two facilities was found, with differences attributable to differences in the flow parameters between the two facilities, particularly the total enthalpy and static temperature, and to the large water content of the vitiation-heated flow.read more
Citations
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Proceedings ArticleDOI
Three-dimensional simulation of thermal choking in a model scramjet combustor
Keith McDaniel,Jack R. Edwards +1 more
Proceedings ArticleDOI
Simulation of thermal choking in a model scramjet combustor
Keith McDaniel,Jack R. Edwards +1 more
Proceedings ArticleDOI
On the bridge from hypersonic aeropropulsion ground test data to flight performance
Three Dimensional Simulation of Time-Dependent Scramjet Isolator/Combustor Flowfields Implemented on Parallel Architectures
TL;DR: McDaniel et al. as discussed by the authors developed a parallel Navier-Stokes solver for computing time-dependent, three-dimensional reacting fields within scramjet (supersonic combusting ramjet) engines.
References
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Book
Molecular theory of gases and liquids
TL;DR: Molecular theory of gases and liquids as mentioned in this paper, molecular theory of gas and liquids, Molecular theory of liquid and gas, molecular theories of gases, and liquid theory of liquids, مرکز
Journal ArticleDOI
Ignition and Combustion Performance of Scramjet Combustors with Fuel Injection Struts
Goro Masuya,Tomoyuki Komuro,Atsuo Murakami,Atsuo Murakami,Noboru Shinozaki,Akihiro Nakamura,Motohide Murayamall,Katsura Ohwaki +7 more
TL;DR: In this article, the performance of a scramjet combustor with a fuel injection strut was experimentally investigated with Mach 2.5 vitiated air, and it was found that mixing and combustion with a less flow-disturbing strut was considerably worse than those with a more flow-disrupting strut.
Journal ArticleDOI
Fuel regression and flame stabilization studies of solid-fuel ramjets
TL;DR: In this article, an experimental investigation of solid-fuel ramjets (SFRJ) has been performed in order to determine the fuel regression behavior and flame stability limits, where the standard fuel in this study was polyethylene (PE), whereas hydroxylterminated polybutadiene (HTPB) fuel was also Investigated in a limited number of tests.