Published June 1, 1957 | Version Published
Project Report Open

Development and application of a technique for steady state aerodynamic heat transfer measurements

Abstract

A technique was developed for measuring steady state heat transfer on a hemisphere cylinder and the results are compared with theory. The instrumentation consisted of a miniaturized thermopile of silver-constantan thermocouples approximately 1/8" x 1/16" x 1/100". The repeatability of readings with this device was found to be excellent. These heat measuring devices, or heat meters, were installed in both a ceramic hemisphere cylinder and in a similar metal one. There were obtained three different heat flow rates at each of six different combinations of tunnel pressure and temperature. The results compared very well with a theory developed by Lester Lees based upon the assumption of local similarity.

Additional Information

Hypersonic Research Project Memorandum, no. 37 - June 1, 1957.

Attached Files

Published - Hartwig_fw_1957.pdf

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Hartwig_fw_1957.pdf

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Additional details

Identifiers

Eprint ID
46905
Resolver ID
CaltechAUTHORS:20140707-143842260

Funding

Army Ordnance Contract
DA-04-495-Ord-19
Army Project
5B0306004
Ordnance Project
TB3-0118
OOR Project
1600-PE

Dates

Created
2014-07-07
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Series Name
Hypersonic Research Project Memorandum
Series Volume or Issue Number
37