"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
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
- United States. National Advisory Committee for Aeronautics (1915-1958) (Publisher, Organization)
- United States. National Advisory Committee for Aeronautics. Ames Aeronautical Laboratory (1939-1958) (Editor, Organization)
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
- Langford, Mark (Donor, Person)
- Aircraft Engine Historical Society, Inc. (Donor, Organization)
Repository Details
Part of the The University of Alabama in Huntsville Archives & Special Collections Repository
M. Louis Salmon Library
301 Sparkman Drive
Huntsville Alabama 35899 United States of America
256-824-6523
archives@uah.edu