Louis S. Stivers

Low-speed tests of five NACA 66-series airfoils having mean lines designed to give high critical Mach numbers

Albert E. von Doenhoff, Louis S. Stivers, James M. O'Connor, 1947 .

Summary of Airfoil Data

Ira H. Abbott, Albert E. von Doenhoff, Louis S. Stivers, 1945 .

The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil

Louis S. Stivers, 1947 .

NATIONAL ADVISORY COMMITI'EE FOR AERONAUTICS

Louis S. Stivers, 1954 .

Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees

Louis S. Stivers, 1954 .