1980•NASA STI Repository (National Aeronautics and Space Administration)Open access

Transonic wing DFVLR-F4 as European test model

Guenter Redeker, N. Schmidt

Abstract

A transonic wing, the DFVLR-F4 was designed and tested as a model in European transonic wind tunnels and was found to give performance improvements over conventional wings. One reason for the improvement was the reduction of compression shocks in the transonic region as the result of improved wing design.

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Key concepts: Transonic, Wing, Subsonic and transonic wind tunnel, Compression (physics), Aeronautics, Aerospace engineering, Engineering, Aerodynamics