MODELING OF DOUBLE CONCENTRIC BURNING JETS
Combustion processes and flame propagation of jet burners
JET↗
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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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SCALING PROBLEMS ASSOCIATED WITH UNSTABLE BURNING IN SOLID PROPELLANT ROCKETS
Scaling in unstable combustion processes of solid propellant rocket engines
SOLID PROPELLANT ROCKET ENGINE↗
THE EFFECT OF A SHOCK WAVE ON A BURNING SOLID PROPELLANT
Combustion instability of solid propellants due to shock waves
COMBUSTION INSTABILITY↗
DRAG COEFFICIENTS OF INERT AND BURNING PARTICLES ACCELERATING IN GAS STREAMS
Drag coefficients of inert and buring metal particles accelerating in gas streams, considering the particles in convective flow behind shock wave in shock tube
GAS STREAM↗
A MATHEMATICAL METHOD TO PREDICT THE EFFECTS OF EROSIVE BURNING IN SOLID-PROPELLANT ROCKETS
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Lenoir, J. M.↗
BURNING RATES OF SOLID PROPELLANTS SECTION REPORT NO. 4-3
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Smith, J. M.↗
Evolution of O stars. III - Helium burning
Evolution of giant star from helium ignition through helium exhaustion - astrophysics
ASTROPHYSICS↗
Evolution II - from the Main Sequence Through Core Helium Burning, M Equals 3M Sun Masses
Evolution of three solar mass star from main sequence to red giant
MAIN SEQUENCE STAR↗
Evolution of O stars. I - Hydrogen burning
O-star evolution from initial main sequence state to point of decreased hydrogen core content
O STAR↗
Statistical Estimation Procedures for the ''burn-in'' Process
Statistical estimation procedures for identifying and eliminating poor quality or defective items
STATISTICAL ANALYSIS↗
Stellar evolution. II - The evolution of a 3 sun-mass star from the main sequence through core helium burning.
Three Sun-mass star evolution from main sequence to helium exhaustion in core, noting chronology of process
ASTRONOMICAL SPECTRUM↗
Evolution of O stars. III - Helium burning.
Stellar evolution for star of 30 solar masses during helium ignition, depletion and exhaustion
HELIUM↗
The effects of chemical and physical parameters on the burning rate of a liquid droplet
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Lorell, J.↗
An investigation of near critical and super- critical burning of fuel droplets Annual report
Combustion characteristics of liquid propellant droplets in air at near critical and super- critical pressures
Dominicis, D. P.↗
The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume analysis
Edelman, R.↗
Burn-rate testing apparatus
Combustibility tester fits into a sealed chamber so that tests may be performed under controlled atmospheric pressure and compostion. Support frame allows rotation of the test sample so that ignition combustion may be tested in various orientations from horizontal to vertical.
Dawn, F. S.↗
Photographic study of solid propellants burning in an acceleration environment Final report
Acceleration effects on aluminized composite solid propellants combustion by high speed color cinematography
Baker, K. L.↗