Accession Number : AD0780758
Title : Evaluation of Airfoil Section Characteristics in Ground Effect.
Descriptive Note : Technical note,
Corporate Author : DAVID TAYLOR MODEL BASIN WASHINGTON D C AERODYNAMICS LAB
Personal Author(s) : Schaeffer,Richard L. ; Fink,Martin D.
Report Date : OCT 1965
Pagination or Media Count : 26
Abstract : The test was begun as an attempt to provide design information on the section characteristics of wings in ground effect. It was found that this objective could not be achieved, so emphasis was shifted to defining trends in the data. The trends showed that profile drag increases as the ground is approached and that the increase is approximately a linear function of height above the ground.
Descriptors : *Airfoils, *Ground effect, Wings, Drag, Lift, Angle of attack, Wind tunnel models
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE