Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings

Jacobs, Eastman N.; Rhode, R. V.

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Title

Main Title Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings
Series Title NACA Technical Reports

Creator

Author: Jacobs, Eastman N.

Creator Type: Personal
Author: Rhode, R. V.

Creator Type: Personal

Contributor

Originator: Langley Aeronautical Laboratory

Contributor Type: Organization

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

Date

Creation: 1938

Language

English

Description

Content Description: From Introduction: "The system presented herein yields, within the limitations of our present knowledge of aerodynamics, a general solution of the resultant wing forces and moments and their distribution. For the sake of completeness and facility in use, the report contains a table of the important section parameters for many commonly used sections and all other necessary data required to solve the most practical design problems coming within the scope of the system."
Physical Description: 31 p. : ill.

Subject

Keyword: airplane designs
Keyword: wings

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: 93R20996
URL: http://hdl.handle.net/2060/19930091706
Report No.: NACA-TR-631
Center for AeroSpace Information Number: 19930091706
Archival Resource Key: ark:/67531/metadc66289