Investigation of Control Signals for Variable Ramps of Twin-Duct Side Inlets
Description:
Report presenting an investigation in the supersonic wind tunnel to determine the effectiveness of experimental control signals applied to a theoretical inlet throat Mach number control system and normal-shock-position control system for varying the inlet geometry of a twin-duct, side-inlet, fuselage forebody model of a prototype aircraft. These types of control systems have been found to be particularly helpful in supersonic flight. Results regarding inlet stability, control requirements, indi…
more
Date:
January 16, 1958
Creator:
Beheim, Milton A. & Yeager, Richard A.
Item Type:
Refine your search to only
Report