Publication Date:
2019-06-28
Description:
Application of computational fluid dynamics to the design and analysis of supercritical wing sections is discussed. Computer programs used to study the flight of modern aircraft at high subsonic speeds are listed and described. The cascades of shockless transonic airfoils that are expected to increase the efficiency of compressors and turbines are included.
Keywords:
AERODYNAMICS
Type:
NASA-CR-155581
Format:
application/pdf