1954•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Flight-determined pressure measurements over the wing of the Douglas D-558-II research airplane at Mach numbers up to 1.14
James R Peele
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Abstract
Report presenting an investigation of the section and panel characteristics and loads obtained from pressure measurements over a 35 degree sweptback wing at level-flight lifts for a range of Mach numbers. Section pressure distributions were taken at the root, midspan, and tip stations of a Douglas D-558-II airplane.