"Method for Calculating the Rolling and Yawing Moments due to Rolling for Unswept Wings With or Without Flaps or Ailerons By Use of Nonlinear Section Lift Data" (NACA Report 1167), 1954

Item — Box: MC-019-001, Folder: 001.A.028

Identifier: 20060154

Staff Only

Scope and Contents

Document Type: Technical Research Report. Authority: Government Civil (authoritative reference). Document Number: National Advisory Committee for Aeronautics (NACA) Report No. 1167, published in 1954.

Scope: NACA research report by Albert P. Martina.

Contents: See title.

Dates

Publication: 1954

Creator

United States. National Advisory Committee for Aeronautics (1915-1958) (Publisher, Organization)
United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory (1917-1958) (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 Volume

Language of Materials

English

Additional Description

Folder Contents

Items in the same folder (ID #s): 20060153, 20060154 & 20060139.

Digital Scan Location

TBD

Format & Physical Description

Format: Stapled booklet with brown cardstock cover, 9.25" x 11.5" (20 pages plus covers, with the last 2 pages blank). Includes black & white graphs and charts. Staples have been removed.

Publication Data

Publication Data: Published by NACA in 1954. "For Sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C." for 20 cents.

Note: Cover marked "B56" in red marker.