Aerofoils -- Testing

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

David E. Hahne and Frank L. Jordan, Jr.

Aerofoil testing in a self-streamlining flexible walled wind tunnel

Mark Charles Lewis.

Transsonische Strömungen an einem schwingenden Profil und deren Einfluss auf die Flattergrenze

Lorenz Tichy.

High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel

Raymond E. Mineck and Pierce L. Lawing.

Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel

Renaldo V. Jenkins

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

Renaldo V. Jenkins, Acquilla S. Hill, and Edward J. Ray.

The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil: suction coefficient analysis

Cuyler W. Brooks, Jr., Charles D. Harris, and William D. Harvey.

Design and experimental results for a Natural-Laminar-Flow airfoil for general aviation application

Dan M. Somers

Design and experimental results for a flapped natural-laminar-flow airfoil for general aviation applications

Dan M. Somers

An experimental evaluation of advanced rotorcraft airfoils in the NASA Ames eleven-foot wind tunnel

Robert J. Fleming.