Results 101 to 110 of about 1,472 (179)

Synchronized Initiation of Two Cylindrical Rotating Detonation Engines [PDF]

open access: yes
A coupled cylindrical rotating detonation engine (RDE) with two cylindrical RDEs (both combustors had a combustor inner diameter of 23 mm and an axial length of 30 mm) placed next to each other was tested for rocket clustering application.
Funaki, Ikkoh   +7 more
core   +1 more source

Institute for Computational Mechanics in Propulsion (ICOMP) [PDF]

open access: yes
The Institute for Computational Mechanics in Propulsion (ICOMP) is a combined activity of Case Western Reserve University, Ohio Aerospace Institute (OAI) and NASA Lewis.
Feiler, Charles E.
core   +1 more source

Impact of an Exhaust Throat on Semi-Idealized Rotating Detonation Engine Performance [PDF]

open access: yes
A computational fluid dynamic (CFD) model of a rotating detonation engine (RDE) is used to examine the impact of an exhaust throat (i.e., a constriction) on performance.
Paxson, Daniel E.
core   +1 more source

Influence of fuel inhomogeneity on detonation wave propagation in a rotating detonation combustor

open access: yesShock Waves
AbstractRotating detonation combustor (RDC) is a form of pressure gain combustion, which is thermodynamically more efficient than the traditional constant-pressure combustors. In most RDCs, the fuel–air mixture is not perfectly premixed and results in inhomogeneous mixing within the domain.
P. Raj, J. Meadows
openaire   +2 more sources

Ejector Enhanced Pulsejet Based Pressure Gain Combustors: An Old Idea With a New Twist [PDF]

open access: yes
An experimental investigation of pressure-gain combustion for gas turbine application is described. The test article consists of an off-the-shelf valved pulsejet, and an optimized ejector, both housed within a shroud.
Dougherty, Kevin T., Paxson, Daniel E.
core   +1 more source

Aero-Propulsion Control Research in Support of NASA Aeronautics Research Strategic Thrusts [PDF]

open access: yes
In the past few years, NASA (National Aeronautics and Space Administration) Aeronautics Research Mission Directorate (ARMD) has introduced and updated a New Blueprint for Transforming Global Aviation .
Garg, Sanjay
core   +1 more source

An investigation of spherical blast waves and detonation waves in a rocket combustion chamber [PDF]

open access: yes
Spherical blast waves and detonation waves in rocket combustion ...
Bonnell, J. M.
core   +1 more source

Aeronautical Engineering: A special bibliography with indexes, supplement 54 [PDF]

open access: yes
This bibliography lists 316 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...

core   +1 more source

Three-dimensional simulation of detonation initiation and propagation in supersonic combustible mixtures

open access: yes, 2014
Detonation initiation and propagation in supersonic combustible mixtures using a hot jet have been investigated in three-dimensional numerical simulations with the detailed reaction model on Tianhe-2 system.
Cai, Xiaodong   +5 more
core  

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