AE2353 WIND TUNNEL TECHNIQUES SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 6TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY SIXTH SEMESTER B.E AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,PREVIOUS YEAR QUESTION PAPERS,MODEL QUESTION PAPERS, CLASS NOTES, IMPORTANT 2 MARKS, 8 MARKS, 16 MARKS TOPICS. IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI, TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2353 WIND TUNNEL TECHNIQUES L T P C
3 0 0 3
OBJECTIVE
To introduce the basic concepts of measurement of forces and moments on models during
the wind tunnel testing.
UNIT I WIND TUNNELS 10
Classification –non-dimensional numbers-types of similarities - Layout of open circuit and
closed circuit subsonic wind tunnels – design parameters-energy ratio - HP calculations.
Calibration.
UNIT II HIGH SPEED WIND TUNNELS 10
Blow down, in draft and induction tunnel layouts and their design features, Transonic,
supersonic and hypersonic tunnels, their peculiarities and calibration. Helium and gun
tunnels, Shock tubes,
UNIT III WIND TUNNEL MEASUREMENTS 12
Pressure,velocity and temperature measurements – Force measurements – types of
balances-Three component and six component balances – calibration of measuring
instruments.
UNIT IV FLOW VISUALIZATION 6
Smoke and Tuft grid techniques – Dye injection special techniques – Optical methods of
flow visualization.
58
UNIT V NON-INTRUSIVE FLOW DIAGNOSTICS 7
Laser – Doppler anemometry. Particle image velocimetry. Laser induced fluorescence.
TOTAL: 45 PERIODS
TEXT BOOK
1. Rae, W.H. and Pope, A. “Low Speed Wind Tunnel Testing”, John Wiley Publication,
1984.
REFERENCE
1. Pope, A., and Goin, L., “High Speed wind Tunnel Testing”, John Wiley, 1985.
AE2353 WIND TUNNEL TECHNIQUES L T P C
3 0 0 3
OBJECTIVE
To introduce the basic concepts of measurement of forces and moments on models during
the wind tunnel testing.
UNIT I WIND TUNNELS 10
Classification –non-dimensional numbers-types of similarities - Layout of open circuit and
closed circuit subsonic wind tunnels – design parameters-energy ratio - HP calculations.
Calibration.
UNIT II HIGH SPEED WIND TUNNELS 10
Blow down, in draft and induction tunnel layouts and their design features, Transonic,
supersonic and hypersonic tunnels, their peculiarities and calibration. Helium and gun
tunnels, Shock tubes,
UNIT III WIND TUNNEL MEASUREMENTS 12
Pressure,velocity and temperature measurements – Force measurements – types of
balances-Three component and six component balances – calibration of measuring
instruments.
UNIT IV FLOW VISUALIZATION 6
Smoke and Tuft grid techniques – Dye injection special techniques – Optical methods of
flow visualization.
58
UNIT V NON-INTRUSIVE FLOW DIAGNOSTICS 7
Laser – Doppler anemometry. Particle image velocimetry. Laser induced fluorescence.
TOTAL: 45 PERIODS
TEXT BOOK
1. Rae, W.H. and Pope, A. “Low Speed Wind Tunnel Testing”, John Wiley Publication,
1984.
REFERENCE
1. Pope, A., and Goin, L., “High Speed wind Tunnel Testing”, John Wiley, 1985.
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