A study of subsonic, two-dimensional wall-interference effect in a perforated wind tunnel with particular reference to the NAL 2m x 2m transonic wind tunnel - inapplicability of the conventional boundary condition
By: Masao Ebihara.
Contributors: National Aerospace Laboratory (Japan)
Series: Technical report of the National Aerospace Laboratory -- TR-252T
Publisher: National Aerospace Laboratory
Published: 1972
Place of publication: Tokyo
Number of pages: 28
Subjects: Interference; Transonic wind tunnels; Wind tunnel walls
Notes: Bibliographical references: p.27-28.