NASA Logo - Web Link to NASA.gov

+ Text Only Site
+ Non-Flash Version
+ Contact Glenn

Go
ABOUT NASA NEWS AND EVENTS MULTIMEDIA MISSIONS MyNASA WORK FOR NASA
Photograph of a five hole probe used to determine flow direction.

This page shows two photographs of a five hole probe. The probe is used for diagnostic wind tunnel testing and in flight testing to determine the flow direction or angularity. At the upper left of the figure, we show a picture of the probe itself. The probe is a bundle of five tubes; a center tube surrounded by four tubes in the shape of a cross. The leading edge of the four outside tubes are cut at a 45 degree angle to the center tube.

At the bottom left is a diagram of the probe with a vertical cut through three of the tubes, shown in blue. The flow of air past the probe makes an angle a with the centerline of the center probe. If the angle was zero, all three probes would act as pitot tubes and transducers at the end of the tubes would record the total pressure of the flow. If the angle is not zero, the probe on the bottom detects a pressure p2 that is different than the pressure p1 on the top. The difference is caused by the dynamic pressure associated with the velocity of the flow. The difference in pressure between the top and bottom probes is some function of the angle of the flow:

p1 - p2 = f (a)

We can determine the form of the function by calibrating the probe. A calibration rig is shown in the picture at the upper right of figure. Axial flow is generated by the flow nozzle. The probe is inserted into the flow and the angle that the probe makes with the flow is varied during the calibration test. A mathematical calibration curve is then generated for the measured difference in pressure as a function of the measured angle.

The diagram at the left shows a vertical cut through three of the tubes. The angle of the flow a is then related to the angle of attack of an aircraft. A similar horizontal cut can be made through the two remaining tubes and the angle of the flow is then related to the yaw angle of an aircraft. A five hole probe can therefore be used to simultaneously provide both pitch and yaw information in a flight test, or to provide the flow angularity in two perpendicular planes in a wind tunnel test. There are three hole probes that can also be used if we are only interested in the flow deflection in one direction.

During a wind tunnel or flight test, the probe is inserted into the flow and aligned relative to some part of the tunnel or aircraft. Using the measurements from the five tubes and the calibration curves, we can determine the deflection of the flow in two perpendicular planes relative to the wind tunnel or aircraft part. In some applications, the probe may be moved through the flow field to develop a complete map of the flow angularity. But in most applications, the probe remains fixed to the tunnel wall, model, or flight vehicle.




Navigation ..

Button to Display Wind Tunnel Index Button to Display Propulsion Index Button to Display Aerodynamics Index
Beginner's Guide Home Page

 

     First Gov Image


+ Inspector General Hotline
+ Equal Employment Opportunity Data Posted Pursuant to the No Fear Act
+ Budgets, Strategic Plans and Accountability Reports
+ Freedom of Information Act
+ The President's Management Agenda
+ NASA Privacy Statement, Disclaimer,
and Accessibility Certification

 

NASA Logo   
Editor: Nancy Hall
NASA Official: Nancy Hall
Last Updated: May 05 2015

+ Contact Glenn