Before you begin, you may want to read the laboratory manual and then experiment manual.

	The overall setup of the wind tunnel.  This experiment introduces the student to the use of Laser Doppler Velocimetry (LDV) as a means of measuring air flow velocities.
	A close-up of the "right" half of the wind tunnel.
	A close-up of the "left" half of the wind tunnel.
	The Spectra Physics 124B 15 mW laser (632.8 nm)
	The section drag of a NACA 0012 airfoil can be determined from velocity measurements obtained in the airfoil wake.
	The 0.5 m x 0.7 m wind tunnel has a maximum velocity of 20 m/s.