NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By: Renaldo V. Jenkins.
Contributors: Langley Research Center
Publisher: Langley Research Center
Published: 1989
Place of publication: Hampton, Va
Number of pages: 55
Subjects: Supercritical airfoils; Wind tunnel walls
Notes: Bibliographical references: p.5-6.