Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
Book details
- Title
- Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
- Publication year listed
- 1929
- Format
- Public domain eBook
- Reading access
- Free online reader; no registration required
- Source record
- View on Archive.org
About this book
Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
Author: Wenzinger, Carl J
Year: 1929
This report deals with pressure distribution tests on an airfoil with a conventional trailing edge flap. These tests were conducted in the Atmospheric Wind Tunnel of the National Advisory Committee for Aeronautics. Maximum chord loadings were obtained with the flap displaced downward and with the airfoil at large angles of attack. Greater changes were produced in the normal force and in the center of pressure travel by up-flap than by an equal down-flap displacement.
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