J. A. Dahlin

Analysis of Mach number 0.8 turboprop slipstream wing/nacelle interactions

H. R. Welge, D. H. Neuhart, J. A. Dahlin, 1981 .

Results of design studies and wind tunnel tests of high-aspect-ratio supercritical wings for an energy efficient transport

P. A. Henne, J. A. Dahlin, D. K. Steckel, 1980 .

Configuration design studies and wind tunnel tests of an energy efficient transport with a high-aspect-ratio supercritical wing

P. A. Henne, J. A. Dahlin, C. C. Peavey, 1982 .