Audiobook
We may earn a commission. Learn more.
Supersonic Lift and Pitching Moment of Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration Subsonic Leading Edges and Supersonic Trailing Edges
Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Reviews
No reviews yet.
Be the first to write one.
Highlights
No highlights yet.
Be the first to share one.