Skip to main content
Advances in Aerodynamics

Table 1 Geometrical dimensions of the NASA CRM CFD model

From: Unsteady shock front waviness in shock-buffet of transonic aircraft

Dimension

–

Ref. Area

389.76 m2

Span

59.226 m

Ref. Chord

7.0005 m

Aspect Ratio

9

Taper Ratio

0.275

25% chord Sweep

35.0 °

Back to article page