Theoretical studies of unsteady transonic flow. Part IV. The oscillating rectangular wing with control surface
By: Marten T. Landahl.
Contributors: Aeronautical Research Institute of Sweden
Series: Flygtekniska Forsoksanstalten. Meddelande -- 80; Aeronautical Research Institute of Sweden. Report -- 80
Publisher: Aeronautical Research Institute of Sweden
Published: 1959
Place of publication: Stockholm
Number of pages: 28
Notes: Bibliographical references: p.21.