Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
Description:
From Introduction: "The present paper employs an approach believed to be novel in slender-body theory and is concerned with developing formulas for the forces and moments as well as the stability derivatives for slender wing-body combinations."
Date:
November 1954
Creator:
Sacks, Alvin H.
Partner:
UNT Libraries Government Documents Department