FREE
AKTU Aerodynamic Design and Testing Lab (BAE652) Syllabus PDF – B.Tech 3rd Year
Aerodynamic Design and Testing Lab BAE652
All syllabus, notes, question bank & PYQ for this subject
Free
Download now
- English
- Semester 6
- 0 downloads
- 0 views
Official AKTU syllabus of Aerodynamic Design and Testing Lab (BAE652) for B.Tech 3rd Year – 1 credits, L-T-P 0-0-2. Read the unit-wise course content, course outcomes, evaluation pattern and recommended books online, or download the PDF.
Syllabus — Aerodynamic Design and Testing Lab
Download PDFBAE652 · 1 credits · L-T-P 0-0-2
| The students will be able to | Blooms Taxonomy | |
| CO-1 | Understand the difference surface control arrangement of elevator, aileron, redder, flaps and spoiler. | K2 |
| CO-2 | Understand the Understand the operation of different types of wind tunnel and its calibration. | K2 |
| CO-3 | Apply the concept of flow visualization studies in low speed flow over airfoil with different angle of incidence. | K3 |
| CO-4 | Apply the concept of Pressure distribution of various airfoils can be identified and lift can be calculated. | K3 |
| CO-5 | Understand the force measurement using wind tunnel balance the velocity of the subsonic wind tunnel at various RPM. | K2 |
| CO-6 | Apply the concept of measurement technique of pressure, velocity, lift and drag forces in wind tunnel. | K3 |
Minimum 10 out of following such experiments (or such experiments)
- To demonstrate the longitudinal, lateral and directional stability.
- To demonstrate the effect of roll control: ailerons and spoilers &yaw control, rudder limiters.
- To demonstrate the effect of pitch control pitch control: elevators and horizontal stabilators & variable stabilizers and canards.
- To demonstrate the effect of high lift devices: slots, slats, flaps etc.
- To demonstrate the effect of drag inducing devices: spoilers, lift dumpers, speed brakes:
- Wind tunnel as a tool, their classification, uses and applications.
- Flow visualization studies over airfoils /Cylinder in Smoke Tunnel.
- Calibration of a subsonic Wind tunnel.
- Measurement of pressure gradient along a wind tunnel.
- Plot lift vs. angle of attack for the given airfoil at various speed.
- Measurement of flow velocity in Wind tunnel by Hotwire Anemometer
- Pressure distribution over a symmetric and cambered aerofoil.
- Measurementofvelocityprofileinfavorableandadversepressuregradient.
- Estimationofforcesanddragactingoverasymmetricalairfoilwithdifferentangleofattack.
- Estimation of forces and drag acting over an unsymmetrical airfoil with different angle of attack.
- Pressure distribution over an airfoil and to find lift and drag.
- Pressure distribution over a 2D cylinder and to find lift and drag.
Ratings & Reviews
No reviews yet — share your experience with this item.