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2009, Cambridge aerospace series, ISBN 9780521838153, Volume 9780521838153, xvi, 253
The renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications... 
Airplanes - Scramjet engines | Airplanes | Scramjet engines
Book
SAE technical paper series, Volume 880932.
... engines with some consideratons on questions raised by the vehicule / engine system integration... 
Scramjet engines | Launch vehicles | Rocket engines
eJournal
SAE technical paper series, Volume 2000-01-5602.
...: combined-cycle airbreathing/rocket engines. TSTO configurations were also established as conventional all-rocket and all-airbreathing engine comparison cases... 
Scramjet engines | Rocket engines
eJournal
SAE technical paper series, Volume 985526.
Transportation aspects of commercial spaceflight in the opening decades of the Twenty-first Century are envisioned. A specific Spaceliner concept is described,... 
Scramjet engines
eJournal
SAE technical paper series, Volume 881202.
Sustained high speed flight cannot be achieved by improvements in traditional turbojet/turbofan propulsion systems. Instead, propulsion cycles optimized for... 
Scramjet engines | Hybrid engines | Rocket engines | Turbojet engines
eJournal
SAE technical paper series, Volume 2005-01-3413.
Spacecraft designs incorporating a propulsion system powered by a more efficient fuel would greatly reduce the oxidizer to payload ratio. This could be... 
Scramjet engines | Propellants | Rocket engines
eJournal
SAE technical paper series, Volume 892314.
The numerical simulation of a three-dimensional turbulent, reacting flow through the entire Langley parametric scramjet engine has been obtained using a piecewise elliptic approach... 
Scramjet engines | Computer simulation | Aerodynamics | Jet engines
eJournal
SAE technical paper series, Volume 932551.
Mach-flow angularity probes were developed for use in scramjet flow path probe rakes. Prototype probes were fabricated to demonstrate the assembly processes... 
Scramjet engines | Performance tests | Engine cooling systems | Jet engines
eJournal
SAE technical paper series, Volume 941168.
The US space program is facing the dilemma of the federal government reducing in size, the Congress asking for lowered costs, and the US market share of... 
Scramjet engines | Launch vehicles | Rocket engines | Turbojet engines
eJournal
SAE technical paper series, Volume 912061.
The present work is aimed at experimentally investigating both the development and the oscillation phenomena of pseudo shock waves in a two dimensional... 
Scramjet engines | Tests and Testing
eJournal
SAE technical paper series, Volume 985527.
.... The concept brings together a unique set of subsystem components to enhance the performance of an advanced combined cycle engine powered SSTO design concept... 
Scramjet engines | Manufacturing processes | Launch vehicles | Spacecraft
eJournal
SAE technical paper series, Volume 921226.
The NASA Langley Research Center plans to cany out realistic full-scale tests of supersonic combustion ramjet engines at its 8-Foot High Temperature Tunnel (HTT... 
Scramjet engines | Thermal testing | Fuel injection
eJournal
SAE technical paper series, Volume 872529.
In 1984 government researchers studied the possibility of an aerospace plane, a vehicle able to take off and land horizontally and reach a low earth orbit.... 
Scramjet engines | Military aircraft | Design Engineering and Styling
eJournal
SAE technical paper series, Volume 900990.
The results of computational investigations carried out to clarify the possibilities of hydrogen scramjet thrust uprating in hypersonic flight (Mf>8) by adding... 
Scramjet engines | Performance tests | Materials properties | Aviation fuels
eJournal
International journal of hydrogen energy, ISSN 0360-3199, 2019, Volume 44, Issue 26, pp. 13895 - 13909
Journal Article
Journal of Propulsion and Power, ISSN 0748-4658, 03/2019, Volume 35, Issue 2, pp. 289 - 302
The installed performance of a rotating detonation engine in a waverider vehicle was investigated... 
HYDROGEN-AIR | DESIGN | AUTOIGNITION TEMPERATURES | SCRAMJET | MODEL | ENGINEERING, AEROSPACE | Angles (geometry) | Spontaneous combustion | Parametric analysis | Pressure recovery | Detonation waves | Volumetric efficiency | Rotation | Forebodies | Mach number
Journal Article
Applied thermal engineering, ISSN 1359-4311, 01/2018, Volume 129, pp. 1538 - 1550
.... The feasibility of mode control in rotating detonation engine is investigated through regulating the global equivalence ratio during the test under different air mass flow rates, chamber lengths... 
Rotating detonation engine | Mode transition | Fuel concentration gradient | Chamber length | Controllable transition | ENERGY & FUELS | AIR | FLOW | ENGINEERING, MECHANICAL | WAVE | MECHANICS | THERMODYNAMICS | HYDROGEN FUELED SCRAMJET | COMBUSTION MODE | Strömningsmekanik och akustik | Energy Engineering | Maskinteknik | Teknik | Fluid Mechanics and Acoustics | Engineering and Technology | Energiteknik | Mechanical Engineering
Journal Article
International journal of hydrogen energy, ISSN 0360-3199, 2016, Volume 41, Issue 25, pp. 10942 - 10960
Efficient cooling technologies are required in hydrogen fueled scramjet engines because of its rather large heat load and relatively small coolant mass flow rate... 
Cooling channel | 3-D | Hydrogen fuel | Parametric analysis | Scramjet engine | ELECTROCHEMISTRY | DESIGN | HEAT-TRANSFER | ENERGY & FUELS | PERFORMANCE | CHEMISTRY, PHYSICAL | FLOW | TEMPERATURE | ROCKET ENGINES | ASPECT-RATIO | CHANNELS | CYCLE | Hydrogen as fuel | Numerical analysis | Hydrogen | Analysis | Wall temperature | Scramjet engines | Supersonic aircraft | Coolants | Aspect ratio | Channels | Regenerative cooling | Optimization
Journal Article
International journal of hydrogen energy, ISSN 0360-3199, 03/2015, Volume 40, Issue 9, pp. 3771 - 3776
Rocket-based combined cycle (RBCC) Engine can significantly reduce the amount of onboard oxidizer required... 
Rocket ejector | Maximum thrust | Thermodynamic cycle | RBCC | ELECTROCHEMISTRY | SCRAMJET | ENERGY & FUELS | PERFORMANCE | CHEMISTRY, PHYSICAL | COMBUSTION MODE | Thermodynamics | Hydrogen as fuel | Hydrogen | Analysis
Journal Article
Proceedings of the Combustion Institute, ISSN 1540-7489, 2017, Volume 36, Issue 2, pp. 2883 - 2891
This paper presents the results of a series of shock tunnel experiments of a hydrocarbon-fuelled, Mach 8 shape-transitioning scramjet engine with a cavity combustor... 
Surrogate fuel | Supersonic combustion | Hydrocarbon | Scramjet | ENGINEERING, CHEMICAL | THERMODYNAMICS | ENERGY & FUELS | FUEL | SCRAMJET COMBUSTOR | FLOW | ENGINEERING, MECHANICAL | Methane | Hydrogen as fuel | Combustion | Hydrogen | Tunnels
Journal Article
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