Theoretical analysis of linked leading-edge and trailing-edge flap-type controls at supersonic speeds
Description:
Report presenting an analysis of the use of linked leading-edge and trailing-edge flap-type controls for the purpose of reducing hinge moments at supersonic speeds. A series of linked controls with supersonic leading and trailing edges on swept and unswept wings has been studied for several Mach numbers by use of the linearized theory of supersonic flows. Results regarding hinge moment and hinge-moment reduction and lift and rolling moment are provided.
Date:
March 1956
Creator:
Yates, E. Carson, Jr.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department