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. 2023/24 - Date 09/07/2024 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 courses 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; part B questions 1 and 2; queries 1, 2 of the first part B exercise; queries 1, 2, 3 of the second part B exercise. Part A 1) Which of the following correlations can be for free convection convection over a plate? A NuD = C1ReC2 D PrC3 B NuD = C1GrC2 D PrC3 C* NuL = C1RaC2 L D NuL = C1PeC2 L BiC3 2) In steady-state, 1D, radial conduction conditions, the general temperature and heat flux profilesT(r) and ˙Q ′′ (r) in a homogeneous, hollow cylinder in which a heat source ˙U ′′′ is present read as (C1> 0): A T = ˙U ′′′ r2 4λ − C1ln(r) + C2, ˙Q ′′ = ˙U ′′′ r 2 + C1λ r B T = − ˙U ′′′ r2 4λ + C1ln(r) − C2, ˙Q ′′ =− ˙U ′′′ r 2 + C1λ r C T = − ˙U ′′′ r2 4λ + C1ln(r), ˙Q ′′ = ˙U ′′′ r 2 D* none of the other answers is correct 3) The net energy flux by radiation between two diffuse, gray, opaque facing planes can be expressed as: A ˙E ′′ 1,2 =−σ (T24−T14) 1 ε1 − 1 ε2 B* ˙E ′′ 1,2 =− σ (T24−T14) 1 ε1 + 1 ε2 − 1 C ˙E ′′ 1,2 =− (ε2−ε1)σ (T24−T14) D ˙E ′′ 1,2 =−σ (T24−T14) ε2−ε1 4) The Richardson dimensionless group is defined as: A* Ri = Gr Re2, where Gr and Re are the Grashof and Reynolds dimensionless groups, respectively B Ri =…
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