Rocket and propulsion systems research -- 专题文献

专题：Rocket and propulsion systems research

This cluster of papers focuses on the development, testing, and analysis of hybrid rocket propulsion systems, including the behavior of fuel regression rates, combustion instabilities, thermochemical erosion, and the use of hydrogen peroxide as an oxidizer. It also explores stability analysis, porous chamber flow dynamics, and the application of hybrid rockets in space launch vehicles.

专题：Rocket and propulsion systems research

最新文献

Study on heat transfer characteristics of supercritical CO2/n-decane composite double triangular regenerative cooling for scramjets

Cooling effect of multi-stage water injection on the rocket thermal environment

Inlet Conditions and Fuel Effects on Structures in Backward-Facing Step Combustor

Thermodynamic analysis of nanofluid with aggregated and non-aggregated nanoparticles

The shock-assisted self-ignition behavior and combustion transition mechanisms in a Mach 8 scramjet combustor

Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges

Privileged Scaffold Hybridization for Rigid Tetracyclic Energetics: Uniting Performance, Stability, and Safety

Numerical Analysis of Factors Affecting NOx Emissions in Hydrogen-Fueled Micromix Combustors

Promoting the ignition and combustion performance of Al/CL-20/AP solid propellant by synergistic effects of graphene-based catalysts and interfacial control

Development and Characterization of Hydrogen Peroxide Gels with Organic Gelling Agents for Use with Microencapsulated Fuels

近5年高被引文献