15 research outputs found
Recommended from our members
NACA Research Memorandums
Report presenting the status of oscillating air forces, including forces, moments, and their respective phase angles for a 45 degree swept wing of aspect ratio 2 and for two bodies of revolution. Derivatives based on available analyses were also demonstrated for those three configurations
Recommended from our members
NACA Technical Notes
Report presenting measurements of the aerodynamic forces and moments acting on a wing-tank configuration, with or without fins, oscillating in pitch about the wing-root midchord
Recommended from our members
NACA Technical Notes
Report presenting some experimental measurements of aerodynamic forces and moments on a simple T-tail configuration oscillating in yaw about an axis through the midchord of the vertical fin. Coefficients regarding the rolling moment of the horizontal stabilizer, rolling moment, yawing moment, and side force of the tail are provided