Informazioni sul documento
- Università
- Politecnico di Milano
- Corso di laurea
- Aerospace Engineering
- Materia
- Heat Transfer and Thermal Analysis
- Classificazione
- Esame · Esame completo
- Contenuto
- Soluzione
- Formato originale
- Testo
- Testo ricercabile
Esame completo di Heat Transfer and Thermal Analysis per il corso di Aerospace Engineering presso Politecnico di Milano. Materiale proveniente dall’archivio storico Studwiz e classificato per la consultazione online.
Esame completo di Heat Transfer and Thermal Analysis per il corso di Aerospace Engineering presso Politecnico di Milano. Materiale proveniente dall’archivio storico Studwiz e classificato per la consultazione online.
Qualità dell’importazione: il testo è stato estratto direttamente dal documento originale.
Passaggi rappresentativi riconosciuti nelle diverse parti del materiale. Il testo completo resta presente nella pagina per la ricerca, mentre l’anteprima compatta rende più semplice la lettura.
Heat Transfer and Thermal Analysis - A.A. 2025/26 - Date 07/07/2026 VERY IMPORTANT: the answers must be written on the “Results” paper sheet, not on this text. Only the “Results” paper sheet must be uploaded and will be evaluated. NOTES: Students attending the 5 CFU course may have some different questions in part A. For the exercise queries, in case none of the multiple-choice answers the exercise matches the result you get, write your own result instead of marking an answer (so that in case we did a mistake and your answer is correct you can get the related points). Students having right to a test reduction should answer only to: all part A questions; queries 1, 2, 3 of the part B exercises. Part A 1) Considering a mesh for a CFD simulation, if the cell faces are aligned with the coordinate axes of the domain, the mesh is defined: ADynamic BOverset CUnstructured D*Structured 2) For a full sphere, homogeneous and isotropic, with heat source, exchanging heat by convection with a fluid at uniform temperature under steady-state conditions, the first integration constant obtained when integrating the one-dimensional Poisson equation is: A*Always zero. BAlways negative. CAlways positive. DPositive if the sphere radius is larger than the critical radius of insulation, negative otherwise. 3) A gray, diffuse, opaque surface having α= 0.7, areaA= 2m 2 and temperature 500 K receives an irradiation equal to 930 W/m2. The total power leaving such surface by radiation is: A6981 W B4961 W C*5519 W DThere are not enough data to calculate it. 4) The general form of the Laplace-Young equation reads: A∆P= 2σ / R B∆P=σ(1/R I −1/RII) C*∆P=σ(1/R I + 1/RII) D∆P=σ / R 5) The Weber number, used for convection with phase change, is defined as? A ρV wD2 C σ2 LV B* ρV w2DC σLV C µLw2D2 C σ3…
Prima pagina del documento.