Wind-tunnel investigation at low speeds to determine flow-field characteristics and ground influence on a model with jet-augmented flaps

Raymond D. Vogler, Thomas R. Turner
naca-tn-4116
Sep 1957


A wind-tunnel investigation has been made at low speeds to determine the flow-field characteristics and ground influence on an airplane model having an untapered, unswept wing with an aspect ration of 8.3 equipped with jet-augmented flaps.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1957/naca-tn-4116.pdf