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Airfoil System for Cruising FlightAn airfoil system includes an airfoil body and at least one flexible strip. The airfoil body has a top surface and a bottom surface, a chord length, a span, and a maximum thickness. Each flexible strip is attached along at least one edge thereof to either the top or bottom surface of the airfoil body. The flexible strip has a spanwise length that is a function of the airfoil body's span, a chordwise width that is a function of the airfoil body's chord length, and a thickness that is a function of the airfoil body's maximum thickness.
Document ID
20150003372
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Shams, Qamar A.
Liu, Tianshu
Date Acquired
March 20, 2015
Publication Date
November 11, 2014
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-12/138,709
Patent Number: US-Patent-8,882,049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,882,049
Patent Application
US-Patent-Appl-SN-12/138,709
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