Bryson, Arthur Earl, Jr. (1952) An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer. NACA Technical Reports, NACA-TR1094. National Advisory Committee for Aeronautics , Washington, DC. https://resolver.caltech.edu/CaltechAUTHORS:20140515-091354583
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Abstract
Report presents the results of interferometer measurements of the flow field near two-dimensional wedge and circular-arc sections of zero angle of attack at high-subsonic and low-supersonic velocities. Both subsonic flow with local supersonic zone and supersonic flow with detached shock wave have been investigated. Pressure distributions and drag coefficients as a function of Mach number have been obtained. The wedge data are compared with the theoretical work on flow past wedge sections of Guderley and Yoshihara, Vincenti and Wagner, and Cole. Pressure distributions and drag coefficients for the wedge and circular-arc sections are presented throughout the entire transonic range of velocities.
| Item Type: | Report or Paper (Report) | ||||||||||||
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| Series Name: | NACA Technical Reports | ||||||||||||
| Issue or Number: | NACA-TR1094 | ||||||||||||
| Record Number: | CaltechAUTHORS:20140515-091354583 | ||||||||||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20140515-091354583 | ||||||||||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||||||||||
| ID Code: | 45759 | ||||||||||||
| Collection: | CaltechAUTHORS | ||||||||||||
| Deposited By: | Ruth Sustaita | ||||||||||||
| Deposited On: | 15 May 2014 19:09 | ||||||||||||
| Last Modified: | 03 Oct 2019 06:35 |
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