Wind-tunnel and Flight Investigations of the Use of Leading-edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 ̊swept-wing Airplane
Sign up to use

We may earn a commission. Learn more.

We may earn a commission. Learn more.

Reviews

No reviews yet.
Be the first to write one.

Highlights

No highlights yet.
Be the first to share one.