The temperature dependence of lineshifts, linewidths and line intensities of methane at low temperatures
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Varanasi, Prasad↗
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Results for “temperature”
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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Self-consistent models of spherical accretion onto black holes. I - One-temperature solutions. II - Two-temperatures solutions with pairs
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Park, Myeong-Gu↗
Temperatures, thermal stress, and shock in heat-generating plates of constant conductivity and of conductivity that varies linearly with temperature
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Manson, S V↗
Measurements of Pressure and Temperature for Appraisal of the Temperature Method of Airspeed Calibration in the Lower Stratosphere
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Lina, Lindsay J↗
Investigation of Temperature Limitation of Various Lubricants for High-temperature 20-millimeter-bore Ball Bearings
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Nemeth, Z N↗
Theory and Design of a Pneumatic Temperature Probe and Experimental Results Obtained in a High-temperature Gas Stream
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Simmons, Frederick S↗
A Method of Computing the Transient Temperature of Thick Walls from Arbitrary Variation of Adiabatic-wall Temperature and Heat-transfer Coefficient
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Hill, P R↗
A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures
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Stowell, Elbridge Z↗
Transient temperature distribution in a two-component semi-infinite composite slab of arbitrary materials subjected to aerodynamic heating with a discontinuous change in equilibrium temperature or heat-transfer coefficient
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Trimpi, Robert L↗
Operating Temperatures of I-40-5 Turbojet Engine Burner Liners and the Effect of Temperature Variation on Burner-liner Service Life
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Duffy, Robert T↗
Relation of Nozzle-blade and Turbine-bucket Temperatures to Gas Temperatures in a Turbojet Engine
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Farmer, J Elmo↗
The influence of inlet air temperature and jacket water temperature on initiating combustion in a high speed compression ignition engine
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Matthews, Robertson↗
Experimental Investigation of Air-cooled Turbine Rotor Blade Temperatures in a Turbojet Engine Operating at Turbine-inlet Temperatures up to 2580 Degrees R and Altitudes of 50,000 and 60,000 Feet
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Slone, Henry O↗
A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures
It is shown that for one material, 7075-Tm aluminum-alloy sheet, the information yielded by the relation for these four applications agrees reasonably well with test data.
Stowell, Elbridge Z↗
Low-Temperature Chemiluminescence From cis-1,4-Polybutadiene, 1,2-Polybutadiene, and trans-Polypentenamer at Temperatures Near Ambient
The chemiluminescence emission at 25-60 C was measured from films of cis-1,4-polybutadiene, 1,2-polybutadiene, and trans-polypentenamer. The polymers were autoxidized previously in air 100 C, or allowed to react with singlet molecular oxygen in solution, and then cast into films. Values of beta(or k(sub d,((1)O2 yields (3)03)/k(sub r)((1)O2 + polymer yields products)) were determined in benzene for cis-1,4-polybutadiene and cis-1,4-polyisoprene, and for model compounds cis-3-hexene and cis-3-methyl-3-hexene by independent methods. The chemiluminescence emission from irradiated films of the polymers containing a dye sensitizer showed a complicated time dependence, and the results depended on the length of irradiation.
Nathan, Richard A.↗
TPVF Cell IV Curve Testing with Varying Black Body Emission Temperatures, Intensities, and Cell Temperature
A TPV GaSb cell was tested as part of an effort to establish a standard method of characterizing such cells.
repeatability↗
Evaluation of JPL Version-5.9.12 Temperature Profiles, Ocean Skin Temperature, Surface Emissivity, and Cloud Cleared Radiances
Slide presentation discusses: (1) Modifications to JPL 5.9.12 compared to V5.9.1, (2) Some results showing that V5.9.12 O, with original water vapor sounding channels, is preferable to V5.9.12 N with Antonia Gambacorta s new water vapor channels. (3) Comparison of V5.9.12, V5.9.12 AO, V5.9.1, and V5.0, (4) Accuracy and yield of channel by channel Quality Controlled clear-column radiances R(sub i) and (5) Plans for Version-7.
Susskind, Joel↗
Temperature-Dependent Refractive Index of Cleartran® ZnS to Cryogenic Temperatures
First, let's talk about the CHARMS facility at NASA's Goddard Space Flight Center: Cryogenic, High-Accuracy Refraction Measuring System (CHARMS); design features for highest accuracy and precision; technologies we rely on; data products and examples; optical materials for which we've measured cryogenic refractive index.
Leviton, Doug↗