David J. Wing

Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle

David J. Wing · NASA Technical Reports Server (NASA) · 1994 · 61 citations · Full text

Aeroacoustics, Unsteady Flow, Two-dimensional Convergent-divergent Nozzle +15

Investigation of hybrid fluidic/mechanical thrust vectoring for fixed-exit exhaust nozzles

Christopher Anderson, Victor Giuliano, David J. Wing et al. · 33rd Joint Propulsion Conference and Exhibit · 1997 · 48 citations

Engineering, Aerospace Engineering, Fluid Mechanics +6

Fluidic scale model multi-plane thrust vector control test results

C. Chiarelli, RAYMOND JOHNSEN, CHIH SHIEH et al. · 29th Joint Propulsion Conference and Exhibit · 1993 · 36 citations

Aperture Nozzle, Aeroacoustics, Engineering +13

NASA Langley and NLR Research of Distributed Air/Ground Traffic Management

Mark G. Ballin, Jacco Hoekstra, David J. Wing et al. · 2002 · 34 citations

Air Transportation, Nasa Langley, Engineering +12

Safety Performance of Airborne Separation: Preliminary Baseline Testing

María Consiglio, Sherwood T. Hoadley, David J. Wing et al. · 7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero Sciences,17th LTA Systems Tech Conf; followed by 2nd TEOS Forum · 2007 · 33 citations · Full text