A note on the generation of a compressible vortex rings using helium as driver gas
PRELIMINARY AERODYNAMIC WING DESIGN OF OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT
A note on the generation of a compressible vortex rings using helium as driver gas
Experimental Investigation of The Ship Response to Bow and Stern Slamming Loads
Analysis of the Flow Dynamics of Compressible Vortex Rings Using Compressible Gases
New F. S. (Italian State Rys.) device for varying brake gear ratio
New F. S. (Italian State Rys.) device for varying brake gear ratio
WIND TUNNEL TEST OF A BLENDED WING BODY UNMANNED AERIAL VEHICLE
COMPRESSIBLE VORTEX LOOPS IN A SHOCK TUBE WITH HELIUM DRIVER
Analysis of the Ship Response to Stern Slamming Loads
Effects of Exit Nozzle Diameter on Compressible Vortex Rings Flow Structure
2007-01-1494 Safety Integrity of Memory Sub-Systems in Automotive Microcontrollers