دورية أكاديمية

SOLUTION OF TRANSIENT HEAT TRANSFER PROBLEMS FOR FLAT PLATES, CYLINDERS, AND SPHERES BY FINITE-DIFFERENCE METHODS

التفاصيل البيبلوغرافية
العنوان: SOLUTION OF TRANSIENT HEAT TRANSFER PROBLEMS FOR FLAT PLATES, CYLINDERS, AND SPHERES BY FINITE-DIFFERENCE METHODS
المؤلفون: Burleson, W G, Eppes, Jr, R
المساهمون: ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE
المصدر: DTIC AND NTIS
سنة النشر: 1965
المجموعة: Defense Technical Information Center: DTIC Technical Reports database
مصطلحات موضوعية: Theoretical Mathematics, Thermodynamics, CURVED PROFILES, HEAT TRANSFER, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC HEATING, AIRFRAMES, CYLINDRICAL BODIES, EQUATIONS, FLAT PLATE MODELS, GUIDED MISSILES, MATHEMATICAL ANALYSIS, NOSE CONES, NUMERICAL METHODS AND PROCEDURES, ONE DIMENSIONAL FLOW, REENTRY VEHICLES, SELECTION, SPHERES, SURFACE TEMPERATURE, THERMAL PROPERTIES, THERMAL STRESSES, solutions(mathematics)
الوصف: This report presents finite-difference (forward) heat transfer equations applicable to transient, radial heat flow in spheres and cylinders and applicable to transient, one-dimensional heat flow in flat plates. By minor manipulations, a single heat transfer procedure can be utilized easily to determine the transient heat flow in all three basic structure configurations. For each skin configuration the accuracy of the finite-difference procedure, compared with exact analytical methods, depends on optimum selection of the calculation time increment and the incremental distance between temperature nodes in relation to the material thermal properties and on the closeness of the approximate temperature gradients to the true gradients.
نوع الوثيقة: text
وصف الملف: text/html
اللغة: English
العلاقة: http://www.dtic.mil/docs/citations/AD0461662Test
الإتاحة: http://www.dtic.mil/docs/citations/AD0461662Test
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=AD0461662Test
حقوق: Approved for public release; distribution is unlimited.
رقم الانضمام: edsbas.B2060207
قاعدة البيانات: BASE