Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
By: Kenichi Rinoie.
Contributors: National Aerospace Laboratory (Japan)
Series: Technical report of National Aerospace Laboratory -- TR-1140T
Publisher: National Aerospace Laboratory
Published: 1992
Place of publication: Tokyo
Number of pages: 16
Subjects: Delta wings; Vortex flaps; Vortex plates
Notes: Includes bibliographical references: p. 16.