A study of methods to increase the lift of supersonic airfoils at low speeds
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Authors
Pollock, Albert David
Reck, Floyd Francis
Subjects
Advisors
Date of Issue
1947
Date
Publisher
California Institute of Technology
Language
en_US
Abstract
This thesis presents a study of the problem of improving the
lift characteristics of a supersonic wing at low speeds. Trailing
edge split flaps, nose flaps , and boundary layer control were investigated
singularly and together using the optimum configuration
of each.
Type
Thesis
Description
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NPS Report Number
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Citation
Distribution Statement
Approved for public release; distribution is unlimited.