Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By: Renaldo Jenkins, Acquilla S. Hill and Edward J. Ray.
Contributors: Hill, Acquilla S.; Ray, Edward J.; Langley Research Center
Publisher: Langley Research Center
Published: 1988
Place of publication: Hampton, Va
Number of pages: 296
Subjects: Cryogenic wind tunnels; Supercritical airfoils
Notes: Bibliographical references: p.258.