Experimental investigation of a simplified 3D high lift configuration in support of CFD validation

Transition in the Infinite Swept Attachment Line Boundary Layer

D. I. A. Poll · Aeronautical Quarterly · 1979 · 218 citations

Engineering, Aerospace Engineering, Physics +17

The Langley 14- by 22-Foot Subsonic Tunnel: Description, Flow Characteristics, and Guide for Users

G. L. Gentry, P. Frank Quinto, Gregory M. Gatlin et al. · 1990 · 89 citations

Engineering, Civil Engineering, Subsea Engineering +16

Advances in overset CFD processes applied to subsonic high-lift aircraft

Stuart E. Rogers, Karlin Roth, Steven M. Nash et al. · 18th Applied Aerodynamics Conference · 2000 · 56 citations

Engineering, Aerospace Engineering, Computational Engineering +11

Areas for future CFD development as illustrated by transport aircraft applications

Philip N. Garner, P. G. Meredith, R. Stoner · 1991 · 53 citations

Engineering, Aerospace Engineering, Mechanical Engineering +14

An overview of the Boeing 777 high lift aerodynamic design

B. N. Nield · The Aeronautical Journal · 1995 · 50 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17