Pressure-Distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation

Description:

Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, 20 degrees, and 40 degrees are presented. The normal force coefficients agree with lift coefficients obtained in previous test of the same model, except for the maximum lifts with flap deflection. Pressure distribution measurements were made at Reynolds Number of about 6,000,000.
Creator(s): Abbott, Ira H
Creation Date: January 1, 1942
Partner(s):
UNT Libraries Government Documents Department
About | Browse this Partner
Collection(s):
National Advisory Committee for Aeronautics Collection
About | Browse this Collection
Technical Report Archive and Image Library
About | Browse this Collection
Usage:
Total Uses: 54
Past 30 days: 3
Yesterday: 0
Creator (Author):
Abbott, Ira H
Pressure-Distribution Measurements of a Model of a Davis Wing Section with Fowler Flap Submitted by Consolidated Aircraft Corporation
Original Creation Date: January 1, 1942
Description:

Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, 20 degrees, and 40 degrees are presented. The normal force coefficients agree with lift coefficients obtained in previous test of the same model, except for the maximum lifts with flap deflection. Pressure distribution measurements were made at Reynolds Number of about 6,000,000.
Language(s):
Subject(s):
Keyword(s): aerodynamics
Contributor(s):
Serial Title: NACA Wartime Reports
Partner:
UNT Libraries Government Documents Department
About | Browse this Partner
Collection:
National Advisory Committee for Aeronautics Collection
About | Browse this Collection
Collection:
Technical Report Archive and Image Library
About | Browse this Collection
Identifier:
Resource Type: Report
Format: Text
Rights:
Access: Public
Statement: No Copyright, Unclassified, Unlimited, Publicly available