Theoretical augmentation of turbine-propeller engine by compressor-inlet water injection, tail-pipe burning, and their combination
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Hensley, Reece V↗
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Results for “Burn”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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An Evaluation of the Soap-bubble Method for Burning Velocity Measurements Using Ethylene-oxygen-nitrogen and Methane-oxygen-nitrogen Mixtures
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Simon, Dorothy M↗
Burning Times of Magnesium Ribbons in Various Atmospheres
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Coffin, Kenneth P↗
Burning Velocities of Various Premixed Turbulent Propane Flames on Open Burners
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Wagner, Paul↗
Stability limits and burning velocities of laminar hydrogen-air flames at reduced pressure
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Fine, Burton↗
A relation between burning velocity and quenching distance
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Potter, A E , Jr↗
A general system for calculating burning rates of particles and drops and comparison of calculated rates for carbon, boron, magnesium, and isooctane
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Coffin, Kenneth P↗
Effect of initial mixture-temperature on burning velocity of hydrogen-air mixtures with preheating and simulated preburning
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Heimel, Sheldon↗
Stability limits and burning velocities for some laminar and turbulent propane and hydrogen flames at reduced pressure
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Fine, Burton↗
Altitude-wind-tunnel Investigations of Thrust Augmentation of a Turbojet Engine Performance with Tail-pipe Burning
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W. A. Fleming↗
Theoretical investigation of thrust augmentation of turbojet engines by tail-pipe burning
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Bohanon, H R↗
Experimental Investigation of Thrust Augmentation of a Turbojet Engine at Zero Ram by Means of Tail-pipe Burning
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Lundin, Bruce T↗
Altitude-wind-tunnel Investigation of Thrust Augmentation of a Turbojet Engine IV : Performance with Tail-pipe Burning and Water Injection
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Dietz, Robert O , Jr↗
Internal Flow and Burning Characteristics of 16-inch Ram Jet Operating in a Free Jet at Mach Numbers of 1.35 and 1.73
The effects of mass-flow ratio on the additive drag and normal-shock position of a single oblique-shock diffuser are presented. Also evaluated is the variation with operating condition of the velocity distribution at the combustion-chamber inlet. A comparison with connected-pipe data is included. Burner performance with a corrugated gutter-grid flame holder is discussed. It is shown that the total-pressure drop across the combustion chamber can be predicted with reasonable accuracy from the computed flame holder and combustion momentum pressure losses.
DIFFUSERS, SUPERSONIC↗
Experimental Investigation of Turbojet-engine Thrust Augmentation by Combined Compressor Coolant Injection and Tail-pipe Burning
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Useller, James W↗
Burning Rates of Single Fuel Drops and Their Application to Turbojet Combustion Process
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Graves, Charles C↗
Evaluation of End- and Radial-burning Solid Fuels in Ram Jets Mounted in a Free Jet at Mach Numbers of 2.0, 2.2, and 2.3
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Bartlett, Walter A , Jr↗
Some Measurements of Boiling Burn-out
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Lowdermilk, Warren H↗