Gas Injection

21 books
Combined tangential-normal injection into a supersonic flowP. S. King
⏱ 12m

Combined tangential-normal injection into a supersonic flow

P. S. King

198912 pp.
Direct Injection SystemsCornel Stan
⏱ 1h 40m

Direct Injection Systems

Cornel Stan

2002100 pp.
Evaluation of water injection effect on NOx formation for a staged gas turbine combustorL. Fan

Evaluation of water injection effect on NOx formation for a staged gas turbine combustor

L. Fan

1996No page data
Fuel-injector/air-swirl characterizationJ. B. McVey

Fuel-injector/air-swirl characterization

J. B. McVey

1988No page data
Advanced, small, high-temperature-rise combustor programS. C. Hunter

Advanced, small, high-temperature-rise combustor program

S. C. Hunter

1974No page data
Mixing of an airblast-atomized fuel spray injected into a crossflow of airMay Y. Leong

Mixing of an airblast-atomized fuel spray injected into a crossflow of air

May Y. Leong

2000No page data
Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressureD. St. John
⏱ 14m

Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure

D. St. John

200014 pp.
Direct InjectionSociety of Automotive Engineers
⏱ 3h 49m

Direct Injection

Society of Automotive Engineers

1998229 pp.
Atomization and dispersion of a liquid jet injected into a crossflow of airJ. E. Seay

Atomization and dispersion of a liquid jet injected into a crossflow of air

J. E. Seay

1996No page data
In-flight imaging of transverse gas jets injected into transonic and supersonic crossflowsKon-Sheng Charles Wang

In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows

Kon-Sheng Charles Wang

1994No page data
Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulationMarc W. Kniskern

Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation

Marc W. Kniskern

1990No page data
Flame tube NOx emissions using a lean-direct-wall-injection combustor conceptRobert R. Tacina

Flame tube NOx emissions using a lean-direct-wall-injection combustor concept

Robert R. Tacina

2001No page data
Montana Board of Oil and Gas Conservation class II underground injection control primacy applicationMontana. Oil and Gas Conservation Division

Montana Board of Oil and Gas Conservation class II underground injection control primacy application

Montana. Oil and Gas Conservation Division

1992No page data
A unique, optically accessible flame tube facility for lean combustor studiesUnknown Author

A unique, optically accessible flame tube facility for lean combustor studies

Unknown Author

1995No page data
Investigation of mixing a supersonic stream with the flow downstream of a wedgeJoseph Sheeley

Investigation of mixing a supersonic stream with the flow downstream of a wedge

Joseph Sheeley

1997No page data
Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanksNeil T. Van Dresar

Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks

Neil T. Van Dresar

1995No page data
Making Cars More Fuel EfficientEcmt
⏱ 1h 22m

Making Cars More Fuel Efficient

Ecmt

200582 pp.
Facies heterogeneity and brine-disposal potential of Miocene barrier-island, fluvial, and deltaic systemsWilliam A. Ambrose
⏱ 35m

Facies heterogeneity and brine-disposal potential of Miocene barrier-island, fluvial, and deltaic systems

William A. Ambrose

199035 pp.
Study of injection of helium into supersonic air flow using Rayleigh scatteringRichard G. Seasholtz

Study of injection of helium into supersonic air flow using Rayleigh scattering

Richard G. Seasholtz

1997No page data
Comparison of techniques for non-intrusive fuel drop size measurements in a subscale gas turbine combustorUnknown Author

Comparison of techniques for non-intrusive fuel drop size measurements in a subscale gas turbine combustor

Unknown Author

1999No page data
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