Stability and control force tests of four- and six-unit wing designs of low aspect ratio and 20 degree triangular plan form Page: 1 of 33
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
AC No. o DI7a
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
Miay 1946 as
Advanse Confdential Report 16D17a
SIABILTT ARD COUTRL CO0B B O FU- AHD
SI-UIT WIM MIei OF IDW AET
RA0O AND 200 MIAAR PlN r
BY John W. Paulsoan, Joseph L. Johnson,
and Elizabeth P.. Varney
langrey Meorial Aeronautioal laboratory
angley Field, Va.
NACA WARTIME REPORTS are reprints of papers originally issued to provide rapid distribution of
advance research results to an authorized group requiring them for the war effort. They were pre-
viously held under a security status but are now unclassified. Some of these reports were not tech-
Anically edited. All have been reproduced without change in order to expedite general distribution.
~~_ __ ___ __ ______
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Varney, Elizabeth P; Paulson, John W & Johnson, Joseph L. Stability and control force tests of four- and six-unit wing designs of low aspect ratio and 20 degree triangular plan form, report, May 1, 1946; (digital.library.unt.edu/ark:/67531/metadc62680/m1/1/: accessed October 17, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.