Combustion chambers
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The concept Combustion chambers represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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Combustion chambers
Resource Information
The concept Combustion chambers represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
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- Combustion chambers
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- nasat
124 Items that share the Concept Combustion chambers
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- Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber
- A comparison of combustor-noise models
- A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms
- A fiber-optic probe design for combustion chamber flame detection applications : design criteria, performance specifications, and fabrication technique
- A gas chromatograph/mass spectrometer system for ultralow-emission combustor exhaust studies
- A gas chromatograph/mass spectrometer system for ultralow-emission combustor exhaust studies
- A modified through-flow ware rotor cycle with combustor bypass ducts
- A radiation solver for the national combustion code
- A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
- A simplified model for detonation based pressure-gain combustors
- A study on strength evaluations of EDNi/EDCu/NARloy-Z bonded joints
- A theoretical and experimental study of turbulent evaporating sprays
- A theoretical and experimental study of turbulent particle-laden jets
- A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE
- AST combustion workshop : diagnostic working group report
- Acoustic database for turbofan engine core-noise sources, volume I, final report
- Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype
- Advanced Turbine Technology Applications Project, ATTAP, Hybrid Vehicle Turbine Engine Technology Support, HVTE-TS, 1993-1994 annual report
- Advanced low emissions subsonic combustor study : final report
- Aerothermal modeling : phase I final report : executive summary
- Alternate-fueled combustor-sector emissions
- Alternate-fueled combustor-sector performance
- Alternate-fueled combustor-sector performance, Part A | Part B, Combustor emissions, Combustor performance
- Analytical fuel property effects : final report, Phase 2, Small combustors
- Application of a modified gas chromatograph to analyze space experiment combustion gases on Space Shuttle mission STS-94
- Application of chimera grid scheme to combustor flowfields at all speeds
- Approximation of engine casing temperature constraints for casing mounted electronics
- Assessment of some atomization models used in spray calculations
- Atomization and dispersion of a liquid jet injected into a crossflow of air : under grant NAG3-1124
- Beta testing of CFD code for the analysis of combustion systems
- Bonding Lexan and sapphire to form high-pressure, flame-resistant window
- Burner liner thermal/structural load modeling
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Comparing a Fischer-Tropsch alternate fuel to JP-8 and their 50-50 blend : flow and flame visualization results
- Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
- Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber
- Computational analyses of the LIMX TBCC inlet high-speed flowpath
- Construction of a direct water-injected two-stroke engine for phased direct fuel injection-high pressure charging investigations : order number, A49222D (LAS), April 1, 1998
- Cooling of rocket thrust chambers with liquid oxygen
- Current status of post-combustor trace chemistry modeling and simulation at NASA Glenn Research Center
- Demonstration test of burner liner strain measuring system
- Detailed results from the flame extinguishment experiment (FLEX) March 2009 to December 2011
- Development of UV optical measurements of nitric oxide and hydroxyl radical at the exit of high pressure gas turbine combustors : final report (March 1995 to March 1998)
- Effects of spent cooling and swirler angle on a 9-point swirl-venturi injector
- Ejector enhanced pulsejet based pressure gain combustors : an old idea with a new twist
- Energy efficient engine component development & integration program : semiannual report no. 7, April 1, 1981 - September 30, 1981
- Evaluation of water injection effect on NOx formation for a staged gas turbine combustor
- Experimental and modeling studies of the combustion characteristics of conventional and alternative jet fuels final report
- Experimental clean combustor program : phase II : final report
- Experimental study of cross-stream mixing in a rectangular duct
- Flame radiation and liner heat transfer in a tubular-can combustor
- Flame tube NOx emissions using a lean-direct-wall-injection combustor concept
- Flow processes in overexpanded chemical rocket nozzles, Part 1, Flow separation
- Fluids and Combustion Facility--fluid integrated rack
- Fluids and combustion facility : fluids integrated rack modal model correlation
- Fluids and combustion facility--combustion integrated rack
- Fluids and combustion facility--fluid integrated rack
- Formed platelet liner construction feasibility
- Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines
- Full-scale turbofan engine noise-source separation using a four-signal method
- Funding and strategic alignment guidance for infusing small business innovation research technology into NASA programs associated with the Human Exploration and Operations Mission Directorate
- High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
- Hybrid propulsion for launch vehicle boosters : a program status update
- Injector mixing efficiency experiments : final report : contract number NAS8-38609 D.O. 159
- Introducing the VRT gas turbine combustor
- Investigations of a combustor using a 9-point swirl-venturi fuel injector : recent experimental results
- Lateral jet injection into typical combustor flowfields
- Long life testing of oxide-coated iridium/rhenium rockets
- Low NOx fuel flexible combustor integration project overview
- Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors
- Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Mixing of multiple jets with a confined subsonic crossflow, Part II, opposed rows of orifices in rectangular ducts
- Modeling of turbulent swirling flows
- Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors
- Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors
- NASA flow field analysis : final report
- NASA one-dimensional combustor simulation : user manual for S1D_ML
- NASA/DERA Collaborative Program : interim report
- NASA/QinetiQ Collaborative Program : final report
- National combustion code parallel performance enhancements
- Near-net shape powder metallurgy rhenium thruster
- Near-net shape powder metallurgy rhenium thruster
- Non-intrusive laser-induced imaging for speciation and patternation in high pressure gas turbine combustors
- Non-intrusive laser-induced imaging for speciation and patternation in high pressure gas turbine combustors
- Nondestructive evaluation of ceramic matrix composite combustor components
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part I, Fuel nozzle/rich-burn zone analysis
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part II, Quick-quench/lean-combustion zones analysis
- Numerical study of stratified charge combustion in wave rotors
- Numerical study of stratified charge combustion in wave rotors
- Optical and probe determination of soot concentrations in a model gas turbine combustor
- Optical characterization of a multipoint lean direct injector for gas turbine combustors : velocity and fuel drop size measurements
- Optimization of jet mixing into a rich, reacting crossflow
- Orbit transfer rocket engine technology program : enhanced heat transfer combustor technology : subtasks I & II, task C.1
- Orbit transfer vehicle engine technology program : OTVE turbopump condition monitoring
- Orbit transfer vehicle engine technology program combustor wall condition monitoring, subtask II, task E.5
- Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project
- Plume diagnostics of the RSRM static firings for the pressure perturbation studies
- Prevention of over-pressurization during combustion in a sealed chamber
- Probabilistic modeling of high-temperature material properties of a 5-harness 0/90 Sylramic fiber/CVI-SiC/MI-SiC woven composite
- Probabilistic modeling of high-temperature material properties of a 5-harness 0/90 Sylramic fiber/CVI-SiC/MI-SiC woven composite
- Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster
- RP-2 thermal stability and heat transfer investigation for hydrocarbon boost engines
- Rapid mix concepts for low emission combustors in gas turbine engines
- Real-time optical fuel-to-air ratio sensor for gas turbine combustors
- Redesign and test of an SSME turbopump for the Large Throat Main Combustion Chamber
- SSME Main Combustion Chamber (MCC) 'hot oil' dewaxing
- Separating direct and indirect turbofan engine combustion noise while estimating post-combustion (post-flame) residence time using the correlation function
- SiC and Si[subscript 3]N[subscript 4] recession due to SiO[subscript 2] scale volatility under combustor conditions
- SiC recession due to SiO2 scale volatility under combustor conditions
- Simultaneous laser raman-rayleigh-LIF measurements and numerical modeling results of a lifted turbulent H2/N2 jet flame in a vitiated coflow
- Spreadsheet calculations for jets in crossflow : opposed rows of inline and staggered holes and single and opposed rows with alternating hole sizes
- Structure of a swirl-stabilized combusting spray
- Ten year operating test results and post-test analysis of a 1/10 segment stirling sodium heat pipe : phase III final report
- The effect of air preheat at atmospheric pressure on the formation of NO[subscript x] in the quick-mix section of an axially staged combustor
- The effect of air preheat at atmospheric pressure on the formation of NO[subscript x] in the quick-mix section of an axially staged combustor
- The structure of dilute combusting sprays
- Time-filtered Navier-Stokes approach and emulation of turbulence-chemistry interaction
- Transition mixing study empirical model report
- Transition mixing study final report
- Turbulent radiation effects in HSCT combustor rich zone : prepared under contract NAS3-26618
- Using the NASA GRC sectored-one-dimensional combustor simulation
- Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/iBdpwdKdENA/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/iBdpwdKdENA/">Combustion chambers</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
