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Problem # 5. Levitation. Mingyu Kang. Team Korea. Phenomenon. Investigate the effect Oscillation Produce the maximum angle of tilt. Force Analysis. Bernoulli. Coanda. Flow Chart. -Oscillation . -Oscillation . Airstream Velocity Profile. Optimization ( Maximum angle of tilt).
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Problem #5 Levitation Mingyu Kang Team Korea
Phenomenon • Investigate the effect • Oscillation • Produce the maximum angle of tilt
Force Analysis Bernoulli Coanda
Flow Chart -Oscillation -Oscillation Airstream Velocity Profile Optimization (Maximum angle of tilt) Drag force Gravity Bernoulli effect Coanda effect (Boundary layer thickness) Momentum flow conservation Gaussian curve distribution Force equilibrium Airstream velocity Mass of ball Oscillation period -Equilibrium Point Oscillation period -Equilibrium Point Pitot tube experiment
Momentum flow conservation of free jet Free jet: Momentum flow is a CONSERVED quantity
Velocity at the Center Assume that the velocity is even at the narrow area of the center. By momentum flow conservation
Experiment: Velocity at the Center Pitot tube anemoemeter
Velocity Profile: Gaussian Curve By momentum flow conservation Assume Gaussian curve profile:
Error Airstream velocity at the opening is weaker at the edge!
Drag Force and - Oscillation
Experiment: -Equilibrium Position Cause of Error Gaussian curve assumption Compression effect
Compression of the Airstream When -displacement is low……
Experiment Setting: Compression of the Airstream Force sensor
Experiment Result: Compression of the Airstream Compression!
Pressure Force and - oscillation
How thick is ? Viscous force No-slip Condition Boundary Layer Thickness ( : kinematic viscosity )
Coanda Effect : Bernoulli effect is the major one!
Motion of the Ball Experiment Theory
Theory: Optimization , that achieves ⇒ OPTIMIZATION!
Experiment: Optimization Maximum Angle of Tilt
Conclusion Velocity Profile Gaussian Curve & Momentum flow Conservation - Oscillation Drag Force - Oscillation Bernoulli + Coanda Pressure Force Optimization ,
Spin of the ball 0.74rev/s=4.65rad/s m/s 8.5m/s (airstream velocity at equilibrium point) Irregular direction Small rotation speed NEGLIGENT!