J. Dagenhart

发表

Crossflow-vortex instability and transition on a 45 deg swept wing

W. Saric, J. Dagenhart, J. Stack, 1989 .

Three-dimensional boundary-layer transition on a swept wing at Mach 3.5

J. A. Masad, L. Cattafesta, J. Dagenhart, 1995 .

An orthogonal coordinate grid following the three-dimensional viscous flow over a concave surface

W. Saric, J. Dagenhart, 1983 .

Two experimental supercritical laminar-flow-control swept-wing airfoils

D. O. Allison, Dennis O. Allison, J. Ray Dagenhart, 1987 .

The Gortler Instability on an Airfoil

Siva M. Mangalam, S. Mangalam, J. Dagenhart, 1985 .

Boundary-layer stability analysis of NLF and LFC experimental data at subsonic and transonic speeds

Robert B. Yeaton, S. Berry, J. Dagenhart, 1987 .

Amplified crossflow disturbances in the laminar boundary layer on swept wings with suction

J. Dagenhart, J. R. Dagenhart, 1981 .

Design considerations of advanced supercritical low drag suction airfoils

Helen L. Reed, W. Pfenninger, H. Reed, 1980 .

Design of a laminar-flow-control supercritical airfoil for a swept wing

D. O. Allison, J. Dagenhart, J. R. Dagenhart, 1978 .

Experiments in Swept-Wing Transition

W. Saric, J. Dagenhart, Marc C. Mousseux, 1990 .