Informazioni sul documento
- Università
- Politecnico di Milano
- Corso di laurea
- Aerospace Engineering
- Materia
- Machine Design
- Classificazione
- Esame · Esame completo
- Contenuto
- Testo d’esame
- Formato originale
- Testo
- Testo ricercabile
Esame completo di Machine Design 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 Machine Design 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.
Exercise 1. Consider the document storage shelves shown in Figure 1, a couple of forces are loaded on the handle, at point A, as P (compressive force) and R (radial force). A pulley at point F is the one for moving the shelf with force F. F is along axis x (fixed in space) , P is along axis y’ and R is along axis x’, the last two forces rotating in space together with the structure (Figure 1). All the forces are constant in magnitude . All the beams are made by the material presented in the table below with a hollow cross -section of external diameter, de=5 mm, and internal diameter di=4.5 mm. At the status, the shaft is rotating at a constant angular speed . Figure 1 It is required to: (1) Determine the values of the force F and the reaction forces (2) Draw the internal forces for the structure, separately for the different loads (F, P and R) Also, ignoring the axial and shear forces: (3) Perform the static assessment for point C on the handle part (ABC) . (4) Perform the fatigue assessment for the support point E on the moved part (CDEF). Data: Loads Fatigue parameters: 𝑅 = 600 𝑁 𝑏2 = 0.85 𝑃 = 200 𝑁 𝑏3 = 0.85 q = 0.9 𝐾𝑡𝑏 = 1.5 (for supports and corner points ) 𝐾𝑡𝑡 = 1.4 (for supports and corner points ) Geometry Material: Ductile steel 𝐴𝐵 = 270 𝑚𝑚 𝜎𝑦 = 276 𝑀𝑃𝑎 𝐵𝐶 = 900 𝑚𝑚 𝜎𝑈𝑇𝑆 = 310 𝑀𝑃𝑎 𝐶𝐷 = 𝐷𝐸 = 𝐸𝐹 = 100 𝑚𝑚 D (diameter of pulley) = 900 mm Politecnico di Milano - Master of Science in Aeronautical Engineering Academic year 20 22-23 Course of Machine Design (Prof. M. Giglio) Written test 1 – June 28, 2023 NAME : SURNAME : Polimi-ID : Do not write here: 1 2 3 Total Exercise 2 The plate shown in the Figure 2 is subjected to a far -field stress composed by σ and τ. A crack with initial length 2𝑎 = 3 𝑚𝑚 is found in the middle of the plate . Assuming 𝜎 = 𝜎0(1 + 𝑠𝑖𝑛(𝜔𝑡)) and…
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