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Dept     : AERO
Sem      : 4
Regul    : 2023
Faculty : K NEHRU
phone  : 9159839050
E-mail  : nehru1991@gmail.com
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  • Resource Link

    Dear Students, the Resource Link has been uploaded for the following topics:</br>Aircraft Structures</br>Aerospace Structural Analysis</br>Aircraft Structures - I</br>https://nptel.ac.in/courses/101105022</br>- AIRCRAFT STRUCTURES</br>Aircraft Structures Basics</br>Aerospace Structures </br>Introduction to Aerospace Flight Vehicles</br>AIRCRAFT STRUCTURES

  • Youtube Video

    Dear Students, the Youtube Video has been uploaded for the following topics:</br>Deflection of cantilever beam due to UDL load for entire space of the beam case</br>Deflection of cantilever beam due to point load case</br>Castigliano’s Theorem</br>Deflection by Strain Energy Method</br>Strain Energy Method in Structural Analysis</br>Method of Sections</br>Truss Maestro - Design Thinking based Student activity </br>Fatigue Life Regime & Fatigue Design</br>Fatigue Fracture - Identifying Fatigue Failure Patterns</br>Fatigue Load – Understanding Cyclic Stresses </br>Fatigue Strength and Analysis</br>Unsymmetrical Bending in Beam-DT Based Student Activity</br>Buckling of Plates and Aircraft Load Analysis</br>Design Thinking Approach to Structural Health Monitoring</br>Impact Loading – Basics & Fundamentals</br>Understanding Thermal Stress – Basics & Fundamentals </br>Case Study on Fatigue Life Evaluation of Airbus A350

  • Assignment

    Assignment topic is Clapeyron’s Three-Moment Equation and due date is 25-02-2025.

  • Assignment

    Assignment topic is Clapeyron’s Three-Moment Equation and due date is 24-02-2025.

  • Resource Link

    Dear Students, the Resource Link has been uploaded for the following topics:</br>EBOOK FUNDAMENTALS OF STRUCTURAL ANALYSIS</br>Aircraft Structures</br>STRUCTURAL ANALYSIS

  • Youtube Video

    Dear Students, the Youtube Video has been uploaded for the following topics:</br>Understanding and Analysing Trusses</br>Method of Joints</br>Tension & Compression Members in Truss Analysis</br>Problem on propped cantilever beam</br>Fixed Beam Carrying a Point Load at the Center</br> Clapeyron's Theorem of Three Moments</br>Unit Load Method