The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique Page: 130 of 174
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to UNT Digital Library by the UNT Libraries Government Documents Department.
Extracted Text
The following text was automatically extracted from the image on this page using optical character recognition software:
7N
NACA TN 302 129
NA CA 63A2/10
-- 20
206
204
PO
f I II I I II
.12
.10
.08
.06
.04
.02
O
.08
.06
.04
.02
0
.12
o .10
.< .08
.06
m .04
S.02
0
.10
.08
.06
.04
.02
.12
.10
.08
.06
.04
.02
.
.I
-- A,
. . 6 - -9 -.,
6 .7 .8 .9 O
Mach number, M
(b) C{, 0./
Figure /4.-Gontinued.
/.1 1.2
- -A,4
-- -
A, 3
Upcoming Pages
Here’s what’s next.
131 of 174
132 of 174
133 of 174
134 of 174
Search Inside
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.
Nelson, Warren H. & Krumm, Walter J. The transonic characteristics of 38 cambered rectangular wings of varying aspect ratio and thickness as determined by the transonic-bump technique, report, June 1955; (https://digital.library.unt.edu/ark:/67531/metadc57496/m1/130/: accessed May 5, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.