Upstream effects of secondary injection on the profiles of a boundary layer over a flat plate.
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Authors
Hofford, Robert Francis.
Subjects
Advisors
Date of Issue
1971-09
Date
September 1971
Publisher
Stanford University
Language
en_US
Abstract
An account is given of the effect on the boundary layer of a secondary
air flow directed normal to a flat plate immersed in a primary
flow field of uniform velocity. System design and tunnel operation are
discussed briefly. Boundary layer profiles are compared to existing
theory and secondary injection effects are discussed.
The work described in this thesis was initiated by the author following
exposure to the field of jet interaction. Boundary layer
conditions during portions of flight where the airstream is subsonic
and jet interaction is the means of control posed the problem considered
herein.
Type
Thesis
Description
This thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library Collection for reasons not now known. It has been included in the digital archive for its historical value to NPS. Not believed to be a CIVINS (Civilian Institutions) title.
Series/Report No
Department
Aeronautics and Astronautics
Organization
Stanford University
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.