List of Experiments / Activities
- Aerodynamic Design and Testing Lab L T P: 0 0 2 Credit: 1
- 1To demonstrate the longitudinal, lateral and directional stability.
- 2To demonstrate the effect of roll control: ailerons and spoilers &yaw control, rudder limiters.
- 3To demonstrate the effect of pitch control pitch control: elevators and horizontal stabilators & variable stabilizers and canards.
- 4To demonstrate the effect of high lift devices: slots, slats, flaps etc.
- 5To demonstrate the effect of drag inducing devices: spoilers, lift dumpers, speed brakes:
- 6Wind tunnel as a tool, their classification, uses and applications.
- 7Flow visualization studies over airfoils /Cylinder in Smoke Tunnel.
- 8Calibration of a subsonic Wind tunnel.
- 9Measurement of pressure gradient along a wind tunnel.
- 10Plot lift vs. angle of attack for the given airfoil at various speed.
- 11Measurement of flow velocity in Wind tunnel by Hotwire Anemometer
- 12Pressure distribution over a symmetric and cambered aerofoil.
- 13Measurementofvelocityprofileinfavorableandadversepressuregradient.
- 14Estimationofforcesanddragactingoverasymmetricalairfoilwithdifferentangleofattack.
- 15Estimation of forces and drag acting over an unsymmetrical airfoil with different angle of attack.
- 16Pressure distribution over an airfoil and to find lift and drag.
- 17Pressure distribution over a 2D cylinder and to find lift and drag.
Course Outcomes (COs)
After completion of the course student will be able to:
- CO1Understand the difference surface control arrangement of elevator, aileron, redder, flaps and spoiler.K2
- CO2Understand the Understand the operation of different types of wind tunnel and its calibration.K2
- CO3Apply the concept of flow visualization studies in low speed flow over airfoil with different angle of incidence.K3
- CO4Apply the concept of Pressure distribution of various airfoils can be identified and lift can be calculated.K3
- CO5Understand the force measurement using wind tunnel balance the velocity of the subsonic wind tunnel at various RPM.K2
- CO6Apply the concept of measurement technique of pressure, velocity, lift and drag forces in wind tunnel. Minimum 10 out of following such experiments (or such experiments)K3
Official AKTU syllabus
This subject is on page 35 of the original AKTU PDF.