Published April 15, 1969 | Version Submitted
Technical Report Open

Finite Disturbance Effect on the Stability of a Laminar Incompressible Wake Behind a Flat Plate

Abstract

An integral method is used to investigate the interaction between the stability of a single frequency finite amplitude disturbance with the non-parallel mean flow in a laminar, incompressible wake behind a flat plate. The mean flow is assumed to be characterized by a few shape parameters. The integrals involving the fluctuating components are determined as functions of those shape parameters by solving the inviscid Rayleigh equation of the linear stability theory using the local mean flow. The variations of the amplitude of the fluctuation and the mean flow in the streamwise direction are then determined from solving the set of ordinary differential equations. The effect of coupling between the mean flow and the fluctuation was found to be very important. The calculations show good agreement with the experimental data of Sato and Kuriki.

Additional Information

Contract No. DA-31-124-ARO(D)-33 U.S. Army Research Office and the Advanced Rsesarch Projects Agency. This research is a part of Project DEFENDER sponsored by the Advanced Research Projects Agency.

Attached Files

Submitted - Finite_Disturbance_Effect_on_the_Stability...Memorandum_No._72.pdf

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Finite_Disturbance_Effect_on_the_Stability...Memorandum_No._72.pdf

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Additional details

Identifiers

Eprint ID
62507
Resolver ID
CaltechAUTHORS:20151201-133700798

Funding

Army Research Office (ARO)
DA-31-124-ARO(D)-33
Advanced Research Projects Agency (ARPA)

Dates

Created
2015-12-03
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
Hypersonic Research Project
Series Name
Hypersonic Research Project Memorandum
Series Volume or Issue Number
72