Development and Testing of a Methane/Oxygen Catalytic Microtube Ignition System for Rocket Propulsion [PDF]
This study sought to develop a catalytic ignition advanced torch system with a unique catalyst microtube design that could serve as a low energy alternative or redundant system for the ignition of methane and oxygen rockets.
Deans, Matthew C., Schneider, Steven J.
core +1 more source
Explore artificial neural networks for solving complex hydrocarbon chemistry in turbulent reactive flows. [PDF]
An J, Qin F, Zhang J, Ren Z.
europepmc +1 more source
Complete computation of turbulent combustion flow involves two separate steps: mapping reaction kinetics to low-dimensional manifolds and looking-up this approximate manifold during CFD run-time to estimate the thermo-chemical state variables.
Chandola, Varun +3 more
core
Numerical Analysis of the Effects of Oxygen-Enriched and Different Inlet Conditions on Performance of an Indirect Reheating Furnace with Pulse Combustion. [PDF]
Gao Q, Pang Y, Sun Q, Liu D, Zhang Z.
europepmc +1 more source
Space Launch System Advanced Development Office, FY 2013 Annual Report [PDF]
The Advanced Development Office (ADO), part of the Space Launch System (SLS) program, provides SLS with the advanced development needed to evolve the vehicle from an initial Block 1 payload capability of 70 metric tons (t) to an eventual capability Block
Bickley, F. P. +2 more
core +1 more source
Some Aspects of Time-Reversal in Chemical Kinetics. [PDF]
Maas U.
europepmc +1 more source
On the alignment of fluid-dynamic principal strain-rates with the 3D flamelet-normal in a premixed turbulent V-flame [PDF]
Beyrau, Frank +5 more
core +1 more source
Prediction of the Number of Patients Infected with COVID-19 Based on Rolling Grey Verhulst Models. [PDF]
Zhao YF, Shou MH, Wang ZX.
europepmc +1 more source
A 5-D Implementation of FGM for the Large Eddy Simulation of a Stratified Swirled Flame with Heat Loss in a Gas Turbine Combustor. [PDF]
Donini A +3 more
europepmc +1 more source
The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor. [PDF]
Gövert S +4 more
europepmc +1 more source

