Results 71 to 80 of about 412,817 (220)
Advanced Energy and Sustainability Research, Volume 7, Issue 9, September 2026.Engineered activated carbon materials with tailored pore structures and surface chemistry deliver high‐performance dual functionality across supercapacitors and hydrogen storage, establishing clear structure–property–performance relationships that advance scalable carbon‐based solutions for next‐generation energy storage and conversion.
Rayhan Hasan Pranto +4 more
wiley +1 more source
Progress of SpaceLiner Rocket-Powered High-Speed Concept [PDF]
, 2013 DLR’s launcher systems analysis division is investigating since a couple of years a visionary, extremely fast passenger transportation concept based on rocket propulsion. Thanks to the multi-national collaboration, the technical lay-out of the SpaceLiner
Lentsch, Aron +3 more
core
MORABA - Overview on DLR's Mobile Rocket Base and Projects [PDF]
, 2012 Mobile Rocket Base (MORABA), a division of the Space Operations and Astronaut Training Department of DLR (Deutsches Zentrum für Luft- und Raumfahrt) provides the national and international scientific community with the opportunity to prepare and ...
Turner, Peter +5 more
core +1 more source
Large Eddy Simulations of gaseous flames in gas turbine combustion chambers [PDF]
, 2012 Recent developments in numerical schemes, turbulent combustion models and the regular increase of computing power allow Large Eddy Simulation (LES) to be applied to real industrial burners.
Staffelbach, Gabriel +2 more
core +1 more source
Energy Science &Engineering, Volume 14, Issue 8, Page 3862-3877, August 2026.This study investigates how iron particles burn across a wide size range, revealing late‐stage nanoparticle release and a previously unrecognised shift in combustion behaviour near 118 µm. High‐speed imaging, PMT diagnostics and SEM analyses have been conducted.
Zakaria Mansouri
wiley +1 more source
, 2021 Rocket Science was commissioned in February 2021 to conduct a scoping exercise to understand bereavement support for people affected by suicide and the needs of people supporting others at risk of suicide in Glasgow City. This report synthesises evidence
Rocket Science UK Ltd
core +1 more source
Mehran University Research Journal of Engineering and Technology, 2019 Optimum characteristic length of the combustion chamber of liquid rocket engine is very important to get higher energy from the liquid propellants. Characteristic length is defined by the time required for complete burning of fuel.
Tajwali Khan, Ihtzaz Qamar
doaj
The flow field in the slender combustion chambers of solid propellant rockets [PDF]
, 2004 We analyse the near inviscid flow field generated in a slender non-axisymmetric cylindrical cavity by the gasification and combustion reactions of a surrounding solid propellant grain.
Liñán Martínez, Amable +2 more
core
Engineering model for rocket exhaust plumes verified by CFD results [PDF]
, 2013 An engineering model (EM) is under development that describes the propagation of a rocket exhaust plume after the nozzle exit. The aim of this EM is to allow a fast analysis of the structure of the plume and the exhaust species within the plume.
Minutolo, Francesco +3 more
core
Flow Separation in Rocket Nozzles, a Simple Criteria [PDF]
, 2005 Cold and hot flow tests were conducted to investigate the flow separation in rocket nozzles. The results are presented. A separation data base including a wide range of literature data is established to evaluate the influence of propellant combination ...
Ralf Stark, Stark, Ralf
core +1 more source