INSTRUMENTATION for Development of AIRCRAFT POWERPLANT COMPONENTS Involving FLUID FLOW

480179

01/01/1948

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
PRESENTED here is a detailed discussion of the measurement requirements of general fluid flow; the design and operational problems of temperature, pressure, and miscellaneous measuring devices; and the development and calibration of various instruments. The complications which distorted and unsteady flow add to the instrument problem are described.
The authors analyze temperature probes to show how their accuracy is affected by radiation, conduction, and gas velocity. A design chart indicates-for various temperature-velocity combinations-which of these sources of error is most serious and what materials are most satisfactory for probes.
Meta TagsDetails
DOI
https://doi.org/10.4271/480179
Pages
13
Citation
Markowski, S., and Moffatt, E., "INSTRUMENTATION for Development of AIRCRAFT POWERPLANT COMPONENTS Involving FLUID FLOW," SAE Technical Paper 480179, 1948, https://doi.org/10.4271/480179.
Additional Details
Publisher
Published
Jan 1, 1948
Product Code
480179
Content Type
Technical Paper
Language
English