Investigation of Horn Balances on a 45 Degree Sweptback Horizontal Tail Surface at High Subsonic Speeds (1948)
NASA Technical Reports Server (NTRS) · leaf 43
NACA EM No . L8j01 1^4 … Figure l4.- Aerodynamic characteristics of the 45° sveptback horizontal tail model equipped vlth the faired horn. M = 0.8o. CONFIDENTIAL
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
