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"The Effectiveness at High Subsonic Mach Numbers of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section" (NACA Technical Note 3127), 1954-03

 Item — Box: MC-019-002, Folder: 001.A.036
Identifier: 20060118

Scope and Contents

Document Type: Technical Research Report. Purpose: Authoritative reference Authority: Government Civil Document Number: NACA Technical Note 3127, dated March 1954.

Scope: Preliminary NACA research report by Louis S. Stivers, Jr. of Ames Aeronautical Laboratory, Moffett Field, Calif.

Contents: See title.

Dates

  • Publication: 1954-03

Creator

Conditions Governing Access

This collection is open for research in the Archives & Special Collections reading room. Handling guidelines and use restrictions will be communicated and enforced by archives staff members.

Extent

1 Issue

Language of Materials

English

Folder Contents

Items in the same folder (ID #s): 20060115, 20060117 & 20060118.

Format & Physical Description

Stapled 8.5" x 11" booklet with tan cardstock covers (16 pages plus covers). Includes black & white graphs and charts. Staples have been removed.

Publication Data

Published by the National Advisory Committee for Aeronautics (NACA) in "Washington, March 1954".

Note: Cover marked "B6" in red marker.

Preservation

Preservation Level 2.F. Digital preservation recommended ASAP.

Source

Repository Details

Part of the The University of Alabama in Huntsville Archives & Special Collections Repository

Contact:
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523