02470oam 2200685 450 991071608150332120210504085828.0(CKB)5470000002517287(OCoLC)785280935(OCoLC)495352125(OCoLC)495355007(EXLCZ)99547000000251728720120408j196812 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierHeat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K /by Jack G. Slaby and William F. MattsonWashington, D.C. :National Aeronautics and Space Administration,December 1968.1 online resource (ii, 22 pages) illustrationsNASA/TN ;D-4959"December 1968."Includes bibliographical references (page 22).CoefficientsnasatSurface temperaturenasatGas flownasatHoneycomb structuresThermodynamicsNuclear fuel elementsDesign and constructionNusselt numberGas flowfastHeatTransmissionfastHoneycomb structuresThermodynamicsfastHydrogenThermal propertiesfastNuclear fuel elementsDesign and constructionfastNusselt numberfastCoefficients.Surface temperature.Gas flow.Honeycomb structuresThermodynamics.Nuclear fuel elementsDesign and construction.Nusselt number.Gas flow.HeatTransmission.Honeycomb structuresThermodynamics.HydrogenThermal properties.Nuclear fuel elementsDesign and construction.Nusselt number.Slaby Jack G.1400713Mattson William F.United States.National Aeronautics and Space Administration,OCLCEOCLCEAD#OCLCQOCLCFOCLCQGPOBOOK9910716081503321Heat-transfer coefficients for hydrogen flowing through parallel hexagonal passages at surface temperatures to 2275 K3548218UNINA