Open Wind Tunnel Manufacturer,Supplier and Exporter in India
Product Code : SCL-CELE-14084
This set of experiments focuses on core principles of aerodynamics
and fluid-structure interaction, typically conducted within a wind
tunnel or similar flow bench apparatus. The primary goal is the empirical
determination of forces and flow characteristics essential for designing
efficient flying vehicles and structures. The analysis moves beyond simple
force measurement to include detailed studies of the flow field, specifically
focusing on the pressure variations over body surfaces, the nature of the boundary
layer, and the structure of the wake downstream of the object.
Furthermore, the inclusion of flow visualization techniques,
particularly in conjunction with a fog generator, allows for the direct
observation of streamlines, which is crucial for understanding complex unsteady
phenomena like flutter.
Objectives: Aerodynamic Measurement and Flow Field
Characterization
|
Objective |
Key Metric / Phenomenon |
Application in Aerodynamics |
|
Determine Drag and Lift Coefficients for Different Models |
Coefficients CD and CL |
Fundamental quantification of forces for aircraft and
vehicle design. |
|
Pressure Distribution on Bodies Immersed in a Flow |
Static Pressure p(x, y) |
Measuring surface pressure to calculate lift, drag, and
moment distributions. |
|
Boundary Layer Analysis |
Boundary Layer Thickness (delta), Separation Point |
Empirical study of the thin layer near the surface where viscosity
effects are dominant. |
|
Investigation of Flutter |
Aeroelastic Instability |
Analyzing the self-excited, sustained oscillation of an
object due to aerodynamic forces. |
|
Wake Measurement |
Velocity Deficit, Turbulence |
Characterizing the turbulent region downstream to calculate
drag indirectly and understand mixing. |
|
In Conjunction with the Fog Generator |
Streamline Visualization |
Using smoke or fog to make instantaneous flow paths visible
for qualitative analysis. |
|
Visualization of Streamlines |
Flow Patterns |
Direct observation of flow separation, reattachment, and
vortex shedding . |
