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Effect of Flow Oscillations on Cavity Drag and a Technique for Their Control

Gharib, M. and Roshko, A. and Sarohia, V. (1985) Effect of Flow Oscillations on Cavity Drag and a Technique for Their Control. JPL Publication, 85-72. . http://resolver.caltech.edu/CaltechAUTHORS:20170726-123311179

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Abstract

The phenomenon of cavity flow oscillation is investigated to determine the conditions for onset of periodic oscillations and to understand the relationship between the state of the shear layer and the cavity drag. Experiments have been performed in a water tunnel using a 4" axisymmetric cavity model instrumented with a strip heater on the nose cone and pressure taps in and around the cavity. A complete set of measurements of oscillation phase, amplitude amplification along the flow direction, distribution of shear stress and other momentum flux is obtained by means of a laser Doppler velocimeter. Drag measurements were made by integrating the mean pressure over the solid surfaces of the cavity. Results indicated exponential cavity drag dependence on the length of the cavity. A jump in the cavity drag coefficient is observed as the cavity flow shows a bluff body wake type behavior. An independent estimate of the drag, which is obtained by integration of shear and mean momentum transfer terms over the peripheral area of the cavity, confirms the exponential dependence of drag on the length of the cavity. Results, also reveal that the drag of the cavity in the non-oscillating mode is less than the case if the cavity were replaced by a solid surface. Natural and forced oscillations of the cavity shear layer spanning the gap are studied. The forced oscillations are introduced by a sinusoidally heated thin-film strip which excites the Tollmein-Schlichting waves in the boundary layer upstream of the gap. For a sufficiently large gap, self-sustained periodic oscillations are observed, while for smaller gaps, which do not oscillate naturally, periodic oscillations can be obtained by external forcing through the strip heater. In the latter case resonance is observed whenever the forcing frequency satisfies phase criterion ψ/2π = N, and amplitude exceeds certain threshold levels, but the phenomenon, is non-self-supporting. The drag of the cavity can be increased by one order of magnitude in the non-oscillating case through external forcing. For naturally occurring oscillations, it is possible for two waves to co-exist in the shear layer (natural and forced). Also, it is possible to completely eliminate mode switching by applying external forcing. For the first time a test is performed to cancel or dampen the amplitude of Kelvin-Helmholtz wave in the cavity shear layer. This is done through introducing an external perturbation with the same frequency of the natural component but having a different phase. Reduction by a factor of 2 is obtained in the amplitude of the oscillation.


Item Type:Report or Paper (Report)
Related URLs:
URLURL TypeDescription
https://ntrs.nasa.gov/search.jsp?R=19860012048OrganizationNASA Technical Reports Server
ORCID:
AuthorORCID
Gharib, M.0000-0002-2204-9302
Additional Information:The research described in this paper was carried out by the Jet Propulsion Laboratory, California Institute of Technology, and was sponsored by the U.S. Army Research Office and the National Aeronautics and Space Administration. Reference herein to any specific commercial product, process, or service by trade name, trade mark, manufacturer, or otherwise, does not constitute or imply its endorsement by the United States Government, or the Jet Propulsion Laboratory, California Institute of Technology. The view, opinions, and/or findings contained in this report are those of the authors and should not be construed as an official Department of the Army position, policy, or decision, unless so designated by other documentation. This effort presents the results of one phase of research carried out at the Jet Propulsion Laboratory, California Institute of Technology, Contract NAS7-918 and sponsored by the U.S. Army Research Office, Contract No. 17134E. We are indebted to Drs. Luis Bernal, for his assistance during the difficult LDV measurement phase, and Dan Nosenchuck, for his assistance during the early strip-heater experiments. Thanks are also due to the technical staff of the Fluid Dynamics Group at JPL, especially to chief technician, Mr. Wayne Bixler, and Messrs. Barney Green, Stan Kikkert, and Robert Smither for their excellent workmanship and assistance in construction of the experimental apparatus.
Funders:
Funding AgencyGrant Number
NASANAS7-918
Army Research Office (ARO)17134E
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JPL Publication85-72
Record Number:CaltechAUTHORS:20170726-123311179
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20170726-123311179
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:79421
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:26 Jul 2017 21:49
Last Modified:26 Jul 2017 21:52

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