Results 71 to 80 of about 4,282 (226)
Thermal-structural design study of an airframe-integrated Scramjet [PDF]
The development and evaluation of a design concept for the cooled structures assembly for the Scramjet engine is discussed. Development concepts for engine subsystems and design concepts for the aircraft/engine interface are included.
Katinszky, E. A. +5 more
core +4 more sources
Application of multi-extruded fuel injectors for mixing enhancement of hydrogen gas at scramjet engine: computational study. [PDF]
Sci Rep, 2023 Abdollahi SA +4 more
europepmc +1 more source
Rocket Based Combined Cycle (RBCC) Propulsion Technology Workshop. Volume 1: Executive summary [PDF]
The goal of the Rocket-Based Combined Cycle (RBCC) Propulsion Technology Workshop was to assess the RBCC propulsion system's viability for Earth-to-Orbit (ETO) transportation systems.
Chojnacki, Kent T.
core +1 more source
Journal of Applied Fluid Mechanics, 2016 A numerical analysis of the inlet-combustor interaction and flow structure through a scramjet engine at a flight Mach number M = 6 with parallel injection (Strut with circular inlet) is presented in the present research article. Three different angles of
K. M. Pandey +2 more
doaj
Total temperature estimation of a hydrogen/air burned-gas torch igniter for a scramjet combustor
Journal of Thermal Science and Technology, 2018 Forced ignition is important for the scramjet engines in supersonic flights. When compared to other forced ignition devices, burned-gas torch igniters are considered suitable for scramjet combustors because it is easy to control the input energy of ...
Tatsuya YAMAGUCHI +5 more
doaj +1 more source
Expanded operational capabilities of the Langley Mach 7 Scramjet test facility [PDF]
An experimental research program conducted to expand the operational capabilities of the NASA Langley Mach 7 Scramjet Test Facility is described. Previous scramjet testing in this facility was limited to a single simulated flight condition of Mach 6.9 at
Guy, R. W., Thomas, S. R.
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Effects of the Fuel Species on the Combustion Pressure in a Two Staged Fueled Scramjet Combustor
AerospaceTwo-staged fuel injection configuration for scramjet combustors has been shown to be effective in distributing heat release in the combustor for preventing the unstart transition of the engine by suppressing peak pressure while increasing the pressure ...
Hironobu Nishiguchi +2 more
doaj +1 more source
Configuration development study of the X-24C hypersonic research airplane [PDF]
Bottom line results were made of a three-phase study to determine the feasibility of designing, building, and operating, and maintaining an air-launched high performance aircraft capable of cruising at speeds up to Mach 8 for short durations. The results
Campbell, D. H. +9 more
core +1 more source
Energies, 2018 This paper aims to contribute to developing a potential combined cycle air-breathing engine integrated into an aircraft design, capable of performing flight profiles on a commercial scale.
Andrew Ridgway +2 more
doaj +1 more source
Transatmospheric vehicle research [PDF]
Research was conducted into the alternatives to the supersonic combustion ramjet (scramjet) engine for hypersonic flight. A new engine concept, the Oblique Detonation Wave Engine (ODWE) was proposed and explored analytically and experimentally.
Adelman, Henry G., Cambier, Jean-Luc
core +1 more source