Numerical lifting line theory applied to drooped leading-edge wings below and above stall /

Numerical lifting line theory applied to drooped leading-edge wings below and above stall /

19

Bibliographic Details
Main Authors: Anderson, John David, Jr. (John David), 1937- 188452, Corda, Stephen, Van Wie, David M.
Format:
Subjects:
Lift (Aerodynamics)

Similar Items