1. Scramjet to ramjet transition in a dual‐mode combustor with fin‐guided injection;Aguilera C.;Proceedings of the Combustion Institute,2017
2. Analysis of dual‐mode hydrocarbon scramjet operation at Mach 4–6.5;Baurle R.A.;Journal of Propulsion and Power,2002
3. Bermejo‐MorenoI. LarssonJ. BodartJ. andVicquelinR.(2013).Wall‐Modeled Large‐Eddy Simulations of the HIFiRE‐2 Scramjet. CTR Annual Research Briefs (LES study).
4. Cabell K. Hass N. StorchA. andGruber M.(2011).HIFiRE direct‐connect rig (HDCR) phase I scramjet test results from the NASA Langley arc‐heated scramjet test facility.AIAA 2011‐2248. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference San Francisco CA(11–14 April 2011).
5. Tests of the JAPHAR dual mode ramjet engine