A 3. A 3. Static Pressure Tip is used. It senses static pressure through radially drilled holes near the tip and can be used in air flow velocities up to 1. FPM. Fig. 1 E shows a Dwyer No. A 3. 05 low resistance Static Pressure Tip. It is designed for use in dust laden air and for rapid response applications. It is recommended where a very low actuation pressure is required for a pressure switch or indicating gage or where response time is critical. Measuring Total Pressure and Velocity Pressure In sensing static pressure we make every effort to eliminate the effect of air movement. To determine velocity pressure, it is necessary to determine these effects fully and accurately. This is usually done with an impact tube which faces directly into the air stream. This type of sensor is frequently called a total pressure pick up since it receives the effects of both static pressure and velocity pressure. In Fig. 2, note that separate static connections A and total pressure connections B can be connected simultaneously across a manometer C. Since the static pressure is applied to both sides of the manometer, its effect is canceled out and the manometer indicates only the velocity pressure. To translate velocity pressure into actual velocity requires either mathematical calculation, reference to charts or curves, or prior calibration of the manometer to directly show velocity. In practice this type of measurement is usually made with a Pitot tube which incorporates both static and total pressure sensors in a single unit. Essentially, a Pitot tube consists of an impact tube which receives total pressure input fastened concentrically inside a second tube of slightly larger diameter which receives static pressure input from radial sensing holes around the tip. The air space between inner and outer tubes permits transfer of pressure from the sensing holes to the static pressure connection at the opposite end of the Pitot tube and then, through connecting tubing, to the low or negative pressure side of a manometer. When the total pressure tube is connected to the high pressure side of the manometer, velocity pressure is indicated directly. See Fig. 3. Since the Pitot tube is a primary standard device used to calibrate all other air velocity measuring devices, it is important that great care be taken in its design and fabrication. In modern Pitot tubes, proper nose or tip design along with sufficient distance between nose, static pressure taps and stem will minimize turbulence and interference. This allows use without correction or calibration factors. All Dwyer Pitot tubes are built to AMCA and ASHRAE standards and have unity calibration factors to assure accuracy. To insure accurate velocity pressure readings, the Pitot tube tip must be pointed directly into parallel with the air stream. As the Pitot tube tip is parallel with the static pressure outlet tube, the latter can be used as a pointer to align the tip properly. When the Pitot tube is correctly aligned, the pressure indication will be maximum. Because accurate readings cannot be taken in a turbulent air stream, the Pitot tube should be inserted at least 8 12 duct diameters downstream from elbows, bends or other obstructions which cause turbulence. To insure the most precise measurements, straightening vanes should be located 5 duct diameters upstream from the Pitot tube.