Thermophysics and Thermal ControlRaymond Viskanta |
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Page 160
... stainless steel . The expres- sion derived for contact conductance is hc = ( km / 80 ) ( 5.22 X 10-68 * + 0.036 P ... stainless - steel and aluminum contacts . stainless - steel equation was based solely on similar metal experimental ...
... stainless steel . The expres- sion derived for contact conductance is hc = ( km / 80 ) ( 5.22 X 10-68 * + 0.036 P ... stainless - steel and aluminum contacts . stainless - steel equation was based solely on similar metal experimental ...
Page 168
Raymond Viskanta. EXPERIMENTAL DATA 1.6 O STAINLESS STEEL TO ZIRCALOY 14 □ ZIRCALOY TO STAINLESS STEEL THEORY BARBER , EQUATION ( 10 ) BARBER , EQUATION ( 13 ) 1.2 CLAUSING , EQUATION ( 8 ) HOLM , EQUATION ( 21 ) STAINLESS STEEL TO ...
Raymond Viskanta. EXPERIMENTAL DATA 1.6 O STAINLESS STEEL TO ZIRCALOY 14 □ ZIRCALOY TO STAINLESS STEEL THEORY BARBER , EQUATION ( 10 ) BARBER , EQUATION ( 13 ) 1.2 CLAUSING , EQUATION ( 8 ) HOLM , EQUATION ( 21 ) STAINLESS STEEL TO ...
Page 172
... stainless - steel contacts , and so its success in evaluating the stainless - steel / zircaloy contact case is not entirely unexpected . Equation ( 24 ) , which was developed from aluminum specimen contact data , was unsatis- factory ...
... stainless - steel contacts , and so its success in evaluating the stainless - steel / zircaloy contact case is not entirely unexpected . Equation ( 24 ) , which was developed from aluminum specimen contact data , was unsatis- factory ...
Contents
Thermal Radiative Properties of Solar Sail Film Materials | 3 |
Infrared Reflectance and Refractive Index of Condensed Gas Films | 22 |
FarInfrared Properties of Baffle Coating Materials | 39 |
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AIAA aluminum analysis angle of attack Astronautics black epoxy paint blanket boundary calorimeter coating coefficient configuration constriction resistance contact area convection cooled correlation cryodeposits cryogen deposit thickness detector determined developed dimensionless dissimilar metal distribution emittance Engineering epoxy equation evaluated experimental film flight frit groove heat flow heat flux heat leak heat loss Heat Transfer heat-transfer heater increase insulation system integral integrating sphere Kapton laser load material MAWD measured microcontacts microsphere MLI system multilayer insulation NASA nodes obtained orbit parameters predicted presented pressure radiation radiative ratio refraction refractive index REYNOLDS ANALOGY sail sample shield shown in Fig solar absorptance solar sail solid Space spacecraft spectral reflectance sphere stainless steel substrate surface Table tank temperature thermal conductivity thermal contact conductance thermal control thermal performance thermocouples Thermophysics tion titania vacuum values view angle wall wavelength ZIRCALOY