ROTORCRAFT WITH POWERPLANT EXHAUST SOUND ATTENUATION

FAN APPARATUS WITH LIFT FAN AND LOUVERED COVER

Exhaust Airflow System

AIRCRAFT LIFTING SURFACE AND AIRCRAFT COMPRISING SUCH LIFTING SURFACE

FLIGHT VEHICLE

Engine strut flow control

AEROELASTIC ADJUSTMENT USING FLUTTER VECTOR STRAIN ENERGY

AIRCRAFT GENERATING LARGER THRUST AND LIFT BY FLUID CONTINUITY

METHODS FOR OPTIMIZING BOUNDARY LAYER CONTROL (BLC) SYSTEMS AND RELATED SYSTEMS

Flow control mechanism for nacelle of turbofan engine

AIRCRAFT WITH RAM AIR TURBINE DISK WITH GENERATOR HAVING BLADE TIP INTEGRATED MAGNETS

Leading edge slat

Arrangement for influencing liquid flow and a method

Aircraft structure and associated tools and methods

EXHAUSTING OF HOT GASES FROM WITHIN AN AIRCRAFT

Ducted wing propulsion system

Aircraft wing with sequentially-timed bellows assembly for optimizing boundary layer control

Aircraft battery system including a pressure-sensitive element sealing a battery venting region from a fluid channel

Aerodynamic element, in particular for aircraft, comprising two aerodynamic parts forming an ascending profile junction

Reaction jet helicopter

Variable-porosity panel systems and associated methods

Propeller-driven helicopter or airplane

Method of and transonically operating aircraft having devices for suppressing aeroelastic instabilities

APPARATUS AND METHOD FOR FLUID MANIPULATION

Leading edge structure for a flow control system of an aircraft

Fan apparatus with lift fan and louvered cover

Method, system and apparatus for reducing fluid drag

SPLIT-TILTWING AIRCRAFT AND RELATED METHODS

Vortex generator system and method for assisting in store separation from a vehicle, and aircraft having vortex generator system

Aircraft generating larger lift by reduction of fluid resistance

Vertical tail unit for flow control

Propeller and propeller blade

Modeling and calculation aerodynamic performances of multi-stage transonic axial compressors

CHARGING STATION AND COMBINED CHARGING STATION

Take-off and landing station

TRANSPORT MODULE

MODULAR AIRCRAFT

Noise abatement systems for retractable leading edge wing slats of an aircraft wing assembly

Aircraft with versatile aviation

Profiled structure and associated turbomachine

WING-TO-BODY TRAILING EDGE FAIRING AND METHOD OF FABRICATING SAME

Aircraft wing with bellows assembly for optimizing a boundary layer control system

Airfoil for flow control including a common inlet/outlet device connected to a porous section

Cooling duct

Rotorcraft equipped with an aerodynamic device having a fairing provided with a perforated plate at an air inlet

Apparatus for reducing drag of a transverse duct exit flow

Cell structure and acoustic attenuation device for a nacelle of an aircraft propulsion assembly

Aerodynamic structure for aircraft wing

Active laminar flow control plenum panel arrangements and installation methods

Cavity acoustic tones suppression

Methods, systems, and apparatuses for in-line variably porous surfaces

Aircraft generating larger lift by reduction of fluid resistance

Aircraft generating larger thrust and lift by fluid continuity

Estimating fluid parameter

Control system

Variable camber system

ROTOR BLADE

Aircraft wing assembly

Air inlet with integrated fluid diverter

Vertical tail unit for flow control

Wing comprising a leading edge having means for preventing the clogging of holes produced in the leading edge

Fluidic device

Leading edge structure for a flow control system of an aircraft

Aircraft and flight control mechanisms used on aircraft

Flight control mechanisms and methods of operating aircraft with flight control mechanisms

Aircraft cabin noise reduction systems and methods

FIXED-WING AIRCRAFT WITH INCREASED STATIC STABILITY

Variable-geometry boundary layer diverter

Leading edge ice-protection system

CONTROL SURFACE COMPONENT FOR A HIGH-LIFT DEVICE OF AN AIRCRAFT AND PRODUCTION METHOD THEREFOR

Airfoil for an aircraft having reduced noise generation

Active flow control systems and methods for aircraft

NACELLE AND METHOD FOR INFLUENCING FLUID FLOWS IN A NACELLE

Sound absorbers for airframe components

Assembly for aircraft comprising engines with boundary layer ingestion propulsion

Structure ensuring attenuation of acoustic waves and thermal exchange

Aircraft or spacecraft fluidic oscillator device

System, Apparatus and Methods for an Airspace Plane with Shockwave Piercing Wings

Gust Alleviator

Tile assembly

Resonant blades using an aperture for cancellation of propeller generated noise

High-lift device of flight vehicle

High-lift device of flight vehicle

Recessed lift spoiler assembly for airfoils

Aerofoil and wings for air vehicles

Airfoil portion with a chamber

Submerged vortex generator

Cavity acoustic tones suppression

Radar energy absorbing deformable low drag vortex generator

Aerodynamic device

Panel for controlling the aerodynamic phenomena on a body

Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element

Profile plate portion for use as an outer wall of a flow body, method for manufacturing a profile plate portion and flow body component comprising a suction-extraction device for fluid

High-lift device of flight vehicle

Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift

Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications

Device for reducing noise from jet-pylon interactions on jet engines

Method of laminar flow control using a door assembly

Active flow control for transonic flight

AIRFOIL WITH FLOW DEFLECTOR

Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow

High-lift system for an aircraft with a main wing and an adjustable slat

Flying object for transonic or supersonic velocities

Surface Ventilator For A Compliant-Surface Flow-Control Device

Door assembly for laminar flow control system

System and method to control flowfield vortices with micro-jet arrays

Establishment of laminar boundary layer flow on an aerofoil body

Method and System for Regulating Internal Fluid Flow Within an Enclosed or Semi-enclosed Environment

Device for Reducing a Drag Produced by the Relative Displacement of a Body and Fluid

MAST 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

Membrane actuator based on ferromagnetic shape memory alloy composite for synthetic jet actuator

Design of membrane actuator based on ferromagnetic shape memory alloy composite for synthetic jet actuator

System for aerodynamic flows and associated method

Method and apparatus for modulating flow separation

System and method to control flowfield vortices with micro-jet arrays

Airship and method of operation

Method and system for regulating fluid over an airfoil or a hydrofoil

Method and system for regulating fluid flow over an airfoil or a hydrofoil

Method and system for regulating pressure and optimizing fluid flow about a fuselage similar body

Slotted aircraft wing

Drag reduction utilizing driven micro-cavities

Wing leading edge architecture suitable for laminar flow

Hybrid (pitot-flush) air intake system for air-breathing missiles and aircraft