72307 ⎘
Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
AIRCRAFT STRUCTURE HAVING AN IMPROVED INLET OPENING FOR ENGINE AIR
#2Flow control ducted fans
#3Engine strut flow control
#4AIRCRAFT GENERATING LARGER THRUST AND LIFT BY FLUID CONTINUITY
#5METHODS FOR OPTIMIZING BOUNDARY LAYER CONTROL (BLC) SYSTEMS AND RELATED SYSTEMS
#6BOUNDARY LAYER SUCTION DESIGN BY USING A CORE OF A WINGTIP VORTEX FOR A LIFT-GENERATING BODY
#7Aircraft wing with sequentially-timed bellows assembly for optimizing boundary layer control
#8Variable-porosity panel systems and associated methods
#9Propeller-driven helicopter or airplane
#10Ice protection and boundary layer suction system for an aircraft aerofoil
#11Vertical tail unit for flow control
#12Propeller and propeller blade
#13Nacelle for an aircraft aft fan
#14Vortex generator passive deployment system
#15VERTICAL-TAILLESS AIRCRAFT
#16Aircraft wing with bellows assembly for optimizing a boundary layer control system
#17Aerodynamic body having perforated skin
#18Methods, systems, and apparatuses for in-line variably porous surfaces
#19Aircraft generating larger thrust and lift by fluid continuity
#20APPARATUS AND SYSTEM FOR DRAG REDUCTION
#21Leading edge structure for a flow control system of an aircraft
#22Simplified fluidic oscillator for controlling aerodynamics of an aircraft
#23Apparatus for laminar flow control
#24Vertical tail unit for flow control
#25Vertical tail unit for flow control
#26Leading edge structure for a flow control system of an aircraft
#27Variable geometry engine inlet for high speed aircraft
#28FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY
#29REDUCED BLADE VORTEX INTERACTION
#30Aerodynamic devices for enhancing lift and reducing drag
#31PASSIVE FLOW CONTROL MECHANISM FOR SUPPRESSING TOLLMIEN-SCHLICHTING WAVES, DELAYING TRANSITION TO TURBULENCE AND REDUCING DRAG
#32CONTROL SURFACE COMPONENT FOR A HIGH-LIFT DEVICE OF AN AIRCRAFT AND PRODUCTION METHOD THEREFOR
#33Airfoil for an aircraft having reduced noise generation
#34Apparatus, system and method for drag reduction
#35Boundary-layer-influencing aerodynamic part and method for producing the same
#36Simplified fluidic oscillator for controlling aerodynamics of an aircraft
#37Aircraft engine nacelle
#38Systems, methods, and apparatuses for airfoil configuration in aircraft
#39Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control
#40Aerofoil and wings for air vehicles
#41Submerged vortex generator
#42Leading edge nose structure on the vertical stabilizer of an aircraft
#43Apparatus and methods for extending hybrid laminar flow control
#44High speed compound rotary wing aircraft
#45Pitching stabilization means and a rotary wing aircraft including such means
#46Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications
#47Wing leading edge venting
#48Method of laminar flow control using a door assembly
#49AIRFOIL WITH FLOW DEFLECTOR
#50Door assembly for laminar flow control system
#51Apparatus, system and method for drag reduction
#52Passive removal of suction air for laminar flow control, and associated systems and methods
#53Apparatus system and method for drag reduction
#54Element for generating a fluid dynamic force
#55Device for Reducing a Drag Produced by the Relative Displacement of a Body and Fluid
#56MAST FOR AN AIRCRAFT NACELLE INCORPORATING MEANS FOR LIMITING THE APPEARANCE OF VIBRATIONS, IN PARTICULAR IN CERTAIN FLIGHT REGIMES, AT A HIGH MACH NUMBER AND LOW LIFT
#57Aerofoils
#58Process for the recovery of the energy from the air in pressurised areas of aircraft
#59Slotted aircraft wing
#60Parasitic drag induced boundary layer reduction system and method