Salt-stress-corrosion cracking of residually stressed ti-8al-1mo-1v brake-formed sheet at 550 deg f /561 deg k/
Salt stress corrosion cracking of residually stressed titanium alloy brake formed sheet for supersonic transport
BRAKE↗
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Results for “K”
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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The coefficient of free turbulence in a jet of atomized liquid fuel <k voprosuo koeffitsiyent svobodnoy turbulentnosti strui raspylennogo zhidkogo topliva<
Free turbulent jet coefficient of atomized liquid fuel jet
FREE JET↗
Tables of the blackbody radiation function. volume i- for wavenumbers from 250 to 2745 cm-1, and temperatures from 150 to 350 deg k
Tables of Planck black body radiation functions in terms of spectral radiance as function of wave number
SPECTRAL EMISSION↗
Thermodynamic properties of cesium up to 1500 deg k
Monomer and dimer cesium thermodynamic properties
CESIUM↗
Hemispherical spectral emittance of ablation chars, carbon, and zirconia /to 3700 deg k/
Hemispherical spectral emission of ablation chars, carbon, and zirconium oxide formed during reentry
ZIRCONIUM OXIDE↗
The present status of very high energy p plus p, p bar plus p, pi plus or minus plus p and k plus or minus plus p scattering
High energy elastic scattering, charge exchange scattering, and polarization experiments
POLARIZATION↗
Fatigue of four stainless steels and three titanium alloys before and after exposure to 550 deg f /561 deg k/ up to 8800 hours
Fatigue tests of stainless steels and titanium alloys before and after exposure to high temperatures
HEAT EFFECT↗
Theory and operation of a variable exposure photographic pyrometer over the temperature range 1800 deg. to 3600 deg f /1255 deg. to 2255 deg. k/
Variable exposure photographic pyrometer - theory and operation
RADIATION EXPOSURE↗
Test plan and test instrumentation, rf test console, appendix k part of the final report
Test plan and instrumentation for radio frequency test console
TEST PROGRAM↗
Thermodynamic and related properties of parahydrogen from the triple point to 100 deg k at pressures to 340 atmospheres
Thermodynamic and related properties of liquid para hydrogen
THERMODYNAMIC PROPERTY↗
Total system noise temperature- 15 deg k.
Noise temperature calculated for traveling wave maser system
NOISE MEASUREMENT↗
Thermodynamic properties of neon from 25 to 300 deg k between 0.1 and 200 atmospheres.
Gaseous and liquid neon thermodynamic properties with extrapolation to temperature and pressure ranges not available from experiment
LIQUID NEON↗
Properties testing of reinforced plastic laminates through the 20 deg k range.
Reinforced plastic laminate test techniques and methods to determine mechanical and thermal properties for structural applications at cryogenic temperatures
MATERIAL TESTING↗
On the electron temperature in the ionosphere in the presence of a constant electric field <k voprosu o temperature elektronov v ionosfere pri nalichii postoyannogo elektricheskogo polya<
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Tsedilina, E. E.↗
On particle flow in the vicinity of a fast moving body <k voprosu o potoke chastits v okresnosti bystro-dvizhushcheyego tela /k teorii zonda/<
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Moskalenko, A. M.↗
Fast response, blackbody furnace for temperatures up to 3000 deg k
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Branstetter, J. R.↗
Experimental investigation of total emittance and solar absorptance of several coatings between 300 deg and 575 deg K
Hemispherical total emittance and solar absorptance characteristics of thermal control coating systems in space nuclear power plant development
NUCLEAR POWER PLANT↗
Containment of liquid zirconium and niobium carbides on graphite between 3500 deg and 4700 deg K
Containment of liquid zirconium and niobium carbides on graphite
NIOBIUM CARBIDE↗