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Wind-tunnel Tests of a Wing with a Trailing-edge Auxiliary Airfoil Used as a Flap

NACA-TN-524 · NASA (NTRS) · 1935

Public domain · NASA (NTRS)Technical Reports

Overview

This report gives the characteristics of a wing with an auxiliary airfoil mounted near its trailing edge and used as a flap. The tests were made with a 10 by 60 inch Clark Y main airfoil and an NACA 0012 flap having a chord equal to 15 percent of the main wing chord. The axis of the flap in all…

Publisher
NASA (NTRS)
Document
NACA-TN-524
Year
1935
Pages
14

Document

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Source & rights

Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

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Document details

Doc number
NACA-TN-524
Publisher
NASA (NTRS)
Year
1935
Pages
14
File size
13 MB