Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range Part 1: Force Tests

Knight, Montgomery; Wenzinger, Carl J.

Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range Part 1: Force Tests Metadata

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Title

Main Title Wind-Tunnel Tests on a Series of Wing Models Through a Large Angle of Attack Range Part 1: Force Tests
Series Title NACA Technical Reports

Creator

Author: Knight, Montgomery

Creator Type: Personal
Author: Wenzinger, Carl J.

Creator Type: Personal

Contributor

Originator: Langley Aeronautical Laboratory

Contributor Type: Organization

Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

Creation: 1930

Language

English

Description

Content Description: "This investigation covers force tests through a large range of angle of attack on a series of monoplane and biplane wing models. The tests were conducted in the atmospheric wind tunnel of the National Advisory Committee for Aeronautics. The models were arranged in such a manner as to make possible a determination of the effects of variations in tip shape, aspect ratio, flap setting, stagger, gap, decalage, sweep back, and airfoil profile. The arrangements represented most of the types of wing systems in use on modern airplanes" (p. 3).
Physical Description: 50 p. : ill.

Subject

Keyword: aircraft wings
Keyword: force characteristics

Collection

Name: National Advisory Committee for Aeronautics Collection

Code: NACA
Name: Technical Report Archive and Image Library

Code: TRAIL

Institution

Name: UNT Libraries Government Documents Department

Code: UNTGD

Rights

Rights Access: public
Rights License: pd
Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available

Resource Type

Report

Format

Text

Identifier

Accession or Local Control No: 93R20677
URL: http://hdl.handle.net/2060/19930091387
Report No.: NACA-TR-317
Center for AeroSpace Information Number: 19930091387
Archival Resource Key: ark:/67531/metadc65972

Note

Display Note: "I."