Citation
McClellan, Robert (1955) Equilibrium Temperature and Heat Transfer Characteristics of Hot Wires in Supersonic Flow. Engineer's thesis, California Institute of Technology. doi:10.7907/AB2Y-MC42. https://resolver.caltech.edu/CaltechETD:etd-12042003-105304
Abstract
An experimental investigation was made of two problems that are fundamental to the application of hot wire anemometry in a supersonic flow. First, the equilibrium temperature of a wire in supersonic flow was established as a function of the flow parameters. Second, the heat loss law for a heated wire in a supersonic flow was determined. In the latter case it was shown that the heat loss, represented by a Nusselt number, is a function of Reynolds number only, with the temperature loading as a parameter. There is no Mach number effect from M = 1.80 to M = 4.54, the range of the present experiments. The results show that the hot wire should be a satisfactory instrument for the measurement of both mean values and fluctuations of the mass flow and the stagnation temperature.
Item Type: | Thesis (Engineer's thesis) |
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Subject Keywords: | Aeronautical Engineering |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 1 January 1955 |
Record Number: | CaltechETD:etd-12042003-105304 |
Persistent URL: | https://resolver.caltech.edu/CaltechETD:etd-12042003-105304 |
DOI: | 10.7907/AB2Y-MC42 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 4766 |
Collection: | CaltechTHESIS |
Deposited By: | Imported from ETD-db |
Deposited On: | 09 Dec 2003 |
Last Modified: | 06 Jul 2023 18:19 |
Thesis Files
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