Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections / Robert E. Berggren and Donald J. Graham.

Saved in:
Bibliographic Details
Main Author: Berggren, Robert E.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Graham, Donald J.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1954.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3172.
Subjects:

PASCAL Offsite

Holdings details from PASCAL Offsite
Call Number: Y 3.N 21/5:6/3172
Y 3.N 21/5:6/3172 Available Place a Hold