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Statistical Analysis of P-10 Field Data by Exposure Levels
None
Date:
September 21, 1951
Creator:
Cell, R. F.
System:
The UNT Digital Library
Flight Investigation at Subsonic, Transonic, and Supersonic Velocities of the Hinge-Moment Characteristics, Lateral-Control Effectiveness, and Wing Damping in Roll of a 60 Degrees Sweptback Delta Wing With Half-Delta Tip Ailerons (Revised)
Report presenting a flight investigation of an NACA hinge-moment roll research model with a sharp-nosed cylindrical body with a cruciform arrangement of 60 degree sweptback delta wings, two of which had half-delta tip controls. Data presented includes the variation with mach number of damping-in-roll coefficient, aileron rolling-moment coefficient, lateral-control effectiveness, and hinge-moment coefficient at various deflections. The rolling effectiveness of this configuration was found to be very satisfactory for a range of speeds.
Date:
September 21, 1951
Creator:
Martz, C. William & Church, James D.
System:
The UNT Digital Library