GARRF

Gopalkrishna Advanced Rural Research Foundation

GARRF • Virtual Engineering Laboratory Manual
Kalam Zero Lab
UTM & Structural Suite
Traditional Physical Lab
₹4.5 Crores+
Requires heavy machinery, hydraulic actuators, and specialized metal test specimens.
Kalam Zero Lab Engine
₹0
Instant access to macro material testing and micro structural mechanics simulations for rural engineering institutions.
Part 1: Vertical Setup — Universal Testing Machine (Macro-Material Testing)

Vertical Floor-Standing UTM Console

Real-time tensile stretching observation displaying live axial load, strain elongation, and ultimate tensile stress telemetry. Pause at any point to analyze fluctuating readings and resume seamlessly.

Axial Load0.0 kN
Engineering Strain0.000
Stress0.0 MPa
StatusRunning
Experiment Description & Theoretical Background: Macro-Material Universal Testing
Macro-Level vs. Micro-Level Integration: This module bridges macro-scale material testing (uniaxial stress-strain behavior of bulk metal specimens) with micro-scale failure analysis (crystalline slip planes and dislocation movements during necking).
Objective: To determine the mechanical properties (Young's Modulus, Yield Strength, Ultimate Tensile Strength, and Percentage Elongation) of various metal specimens under axial tensile loading.
Student Assessment & Viva Questions
Q1. Why does cross-sectional thinning (necking) occur prior to final fracture in ductile metals like structural steel?

Answer Guidance: Once the ultimate tensile strength is reached, plastic deformation becomes unstable and localizes at the weakest point along the specimen length, causing rapid cross-sectional area reduction before separation.

Q2. How does changing the specimen diameter from 10 mm to 16 mm affect the recorded ultimate breaking load?

Answer Guidance: The ultimate load increases proportionally with the cross-sectional area ($A = \frac{\pi d^2}{4}$), requiring higher total force to fracture a thicker bar even though ultimate stress remains a material constant.

Part 2: Horizontal Setup — Micro/Macro Structural Mechanics Suite (8 Loading Regimes)
Structural Lab Controls
Beam, Load Points & Diagrams
Reaction RA--
Reaction RB--
Max Bending (Mmax)--
Max Deflection (δmax)--
Comprehensive Reference: The 8 Structural Loading Regimes
Exp # Loading Regime Primary Mechanics Domain Physical Reality Simulated AI Assistant (SitaRam) Prompt Target
1Single Point LoadStatics / Basic MechanicsSingle heavy axle, crane hook, or concentrated machine mount."SitaRam, explain why maximum bending moment occurs directly under the point load."
2Multiple Point LoadsBridge & Chassis DesignMulti-axle semi-trucks traversing bridges; multiple machine feet on a beam."SitaRam, guide me on how to apply the principle of superposition here."
3UDL (Distributed)Structural Civil & AerospaceSelf-weight of concrete girders, snow accumulation, wing lift forces."SitaRam, derive why the bending moment curve is parabolic for a UDL."
4UVL (Varying)Hydraulic & GeotechnicalRetaining wall hydrostatic pressure, grain silo side-wall pressures."SitaRam, how do I calculate the centroid of a triangular loading diagram?"
5Combined LoadingRealistic Design EngineeringBeam self-weight combined with heavy overhead equipment loads."SitaRam, check my SFD and BMD governing equations for this mixed loading state."
6Moving / Rolling LoadTransportation & Rail MechanicsTrains crossing railway bridges; gantry cranes traversing shop floors."SitaRam, generate the Influence Line Diagram (ILD) for maximum shear at mid-span."
7Impact / Sudden LoadingShock & Vibration EngineeringDropped heavy object, blast loading, automotive bumper shock loading."SitaRam, help me extract the damping ratio from the smartphone accelerometer decay graph."
8Cyclic / Harmonic LoadingMachine Dynamics & FatigueUnbalanced rotating motors, earthquake ground motion, dynamic fatigue."SitaRam, assist me in plotting the frequency response curve and identifying resonance."
Experiment Description & Theoretical Background: Beam Bending & Shear
Micro/Macro Structural Context: Evaluates macro-level support reactions and load distribution combined with micro-level fiber curvature stresses across the beam cross-section.

Simply Supported — Point Load

Max Bending Moment:M_max = PL / 4
Max Deflection:δ_max = PL³ / (48EI)

Simply Supported — UDL

Max Bending Moment:M_max = wL² / 8
Max Deflection:δ_max = 5wL⁴ / (384EI)
Student Assessment & Viva Questions
Q1. What is the physical significance of zero shear force locations along a horizontal beam span?

Answer Guidance: The bending moment reaches its absolute maximum or minimum value at points where the internal shear force crosses zero ($V = 0$).

Q2. How does increasing the Flexural Rigidity ($EI$) impact maximum beam deflection under identical loading?

Answer Guidance: Deflection is inversely proportional to $EI$. Doubling the flexural rigidity cuts the maximum transverse deflection in half.