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Linear instability of far-wake flow

Behrens, Wilhelm and Kubota, Toshi (1970) Linear instability of far-wake flow. AIAA Journal, 8 (6). pp. 1178-1179. ISSN 0001-1452. https://resolver.caltech.edu/CaltechAUTHORS:20170807-141808618

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Abstract

Measurements of the mean wake flow behind circular cylinders at Mach 6, described in Ref. 1, showed that in a certain Reynolds number range (Re_d ≃ 300-4000) the inner wake stemming from the body boundary layers is laminar and loses its identity within 60 diam, and the outer wake, stemming from the bow shock, is also laminar within a certain downstream distance, and may be calculated from a laminar linear theory, but does not become similar (Gaussian) within 2400 diam. Experimental study of the stability of these wakes is presented in Ref. 2.


Item Type:Article
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/3.5868DOIArticle
https://arc.aiaa.org/doi/10.2514/3.5868PublisherArticle
Additional Information:© 1970 AIAA. Received March 5, 1970. This work was carried out under the sponsorship and with the financial support of the U.S. Army Research Office and the Advanced Research Projects Agency under Contract DA-31-124-ARO(D)-33, part of Project DEFENDER sponsored by the Advanced Research Projects Agency.
Funders:
Funding AgencyGrant Number
Advanced Research Projects Agency (ARPA)DA-31-124-ARO(D)-33
Issue or Number:6
Record Number:CaltechAUTHORS:20170807-141808618
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20170807-141808618
Official Citation:Linear instability of far-wake flow W. BEHRENS and T. KUBOTA AIAA Journal 1970 8:6, 1178-9
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:79859
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:07 Aug 2017 21:28
Last Modified:03 Oct 2019 18:24

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