Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel

An edition of Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-Meter Transonic Cryogenic Tunnel (1988)

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

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1988

Publisher

Langley Research Center

Language

Pages

296

Description:

subjects: Cryogenic wind tunnels, Supercritical airfoils