Simple procedure results in more accurate span loadings, lift curve slopes, and spanwise centers of pressure being read directly from charts of NACA Report 921, indexed in Engineering Index 1951 p 45.
Correction of additional span loadings computed by WEISSINGER seven-point method for moderately tapered wings of high aspect ratio
NACA -- Tech Note
1955
31 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1947
|