Composite Materials

102609
Back to Composite Materials

Module 2: Lamina Assumptions and Properties

  1. Q.1(d). The Rule of Mixtures is used to determine (i) Hardness only (ii) Composite properties from constituent properties (iii) Tool wear (iv) Surface roughness20262m

    Module 2: Lamina Assumptions and Properties

    The Rule of Mixtures is used to determine

    (i) Hardness only

    (ii) Composite properties from constituent properties

    (iii) Tool wear

    (iv) Surface roughness

    View this question on its own page →
  2. Q.1(e). A lamina is (i) Single layer of composite material (ii) Multi-layer composite (iii) Matrix material alone (iv) Fiber bundle20262m

    Module 2: Lamina Assumptions and Properties

    A lamina is

    (i) Single layer of composite material

    (ii) Multi-layer composite

    (iii) Matrix material alone

    (iv) Fiber bundle

    View this question on its own page →
  3. Q.3(a). State the assumptions of lamina theory and derive the generalized Hooke's law for an orthotropic lamina.20267m

    Module 2: Lamina Assumptions and Properties

    State the assumptions of lamina theory and derive the generalized Hooke's law for an orthotropic lamina.

    View this question on its own page →
  4. Q.3(b). Explain the orthotropic stiffness matrix and transformed stiffness matrix for composite lamina.20267m

    Module 2: Lamina Assumptions and Properties

    Explain the orthotropic stiffness matrix and transformed stiffness matrix for composite lamina.

    View this question on its own page →
  5. Q.4(a). Discuss the Rule of Mixtures and its significance in predicting composite properties.20267m

    Module 2: Lamina Assumptions and Properties

    Discuss the Rule of Mixtures and its significance in predicting composite properties.

    View this question on its own page →
  6. Q.4(b). Explain transformation matrices and their use in stress-strain transformation.20267m

    Module 2: Lamina Assumptions and Properties

    Explain transformation matrices and their use in stress-strain transformation.

    View this question on its own page →
  7. Q.5(a). A composite has fiber strength of 2500 MPa and matrix strength of 60 MPa. Fiber volume fraction is 0.7. Determine longitudinal strength.20267m

    Module 2: Lamina Assumptions and Properties

    A composite has fiber strength of 2500 MPa and matrix strength of 60 MPa. Fiber volume fraction is 0.7. Determine longitudinal strength.

    View this question on its own page →