Design features and characteristics of conventional, modified and shielded total‐pressure probes are briefly discussed, and compared with new shielded instruments of simple construction which combine smallness of size with adequately fast response to pressure changes. Tests at air speeds up to 280 ft./sec. showed that a probe featuring a total‐traversing cylinder with single orifice inside a tubular shield will register total pressure to within 1 per cent of the dynamic pressure up to inclinations of the flow of ±28 deg., the error in the range ±22 deg. being less than 0.5 per cent. The response time of the instrument under a suddenly applied air pressure of 500 mm. W.G. was less than 60 seconds when linked to a Betz projection manometer. If the inner cylinder is replaced by a central sting, the range of insensitivity to flow inclinations is increased to ±45 deg., the error being less than 0·5 per cent of the dynamic pressure. The response time of this probe under 500 mm. W.G. air pressure was approximately 100 seconds. Still simpler versions of the instruments described are under development.
Article navigation
Review Article|
October 01 1958
Simple Shielded Total‐Pressure Probes: Details of Small Probes with Results of Tests on their Performance
F.A.L. Winternitz, Dipl.Ing.E.T.H., V.D.I.
F.A.L. Winternitz, Dipl.Ing.E.T.H., V.D.I.
Fluid Mechanics Division, Mechanical Engineering Research Laboratory, East Kilbride, Glasgow.
Search for other works by this author on:
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1958
Aircraft Engineering (1958) 30 (10): 313–317.
Citation
Winternitz F (1958), "Simple Shielded Total‐Pressure Probes: Details of Small Probes with Results of Tests on their Performance". Aircraft Engineering, Vol. 30 No. 10 pp. 313–317, doi: https://doi.org/10.1108/eb033029
Download citation file:
161
Views
New and popular articles
Suggested Reading
Probe Measurements in Three‐Dimensional Flow: A Comparative Survey of Different Types of Instrument
Aircraft Engineering (August,1956)
Loss of Momentum and Drag: A Method of Measuring the Drag by Exploration of the Wake Behind a Wing
Aircraft Engineering (January,1937)
Manometers for Routine Testing
Aircraft Engineering (April,1942)
RECOVERY OF FUEL FROM OILY WASTES
Anti-Corrosion Manual (June,1974)
Correspondence: Total Pressure Probes — Kinetic Heating of Thin Wings
Aircraft Engineering (January,1959)
Related Chapters
AN EXAMINATION OF PSYCHOLOGICAL CHARACTERISTICS AND ENVIRONMENTAL INFLUENCES OF FEMALE COLLEGE STUDENTS WHO CHOOSE TRADITIONAL VERSUS NONTRADITIONAL ACADEMIC MAJORS
Advances in Library Administration and Organization
CHAPTER IV TESTING-MACHINES
The testing of materials of construction: a text-book for the engineering laboratory and a collection of the results of experiment.
3. Methods
Specification for tunnelling
Recommended for you
These recommendations are informed by your reading behaviors and indicated interests.
