72030 ⎘
Influencing air-flow over aircraft surfaces, not otherwise provided for by generating shock waves
SYSTEMS AND METHODS FOR PRODUCING TRAVELING WAVES ALONG SURFACES EXPOSED TO SUPERSONIC FLUID FLOWS
#2Systems and methods for producing traveling waves along surfaces exposed to supersonic fluid flows
#3METHOD OF DESIGNING AN AIRCRAFT SHAPE OF A SUPERSONIC AIRCRAFT, METHOD OF PRODUCING A SUPERSONIC AIRCRAFT, AND SUPERSONIC AIRCRAFT
#4Method of and transonically operating aircraft having devices for suppressing aeroelastic instabilities
#5AERODYNAMIC TECHNIQUES AND METHODS FOR QUIETER SUPERSONIC FLIGHT
#6Flow body for an aircraft with a selectively activatable shock bump
#7Aircraft portion with reduced wave drag
#8Flow control method and rotary wing unit
#9Rotating detonation propulsion system
#10Shock wave suppression device and aircraft
#11Method of reducing low energy flow in an isolator of a flight vehicle air breathing engine
#12Method of designing a shape of an airframe of a supersonic aircraft, production method of a supersonic aircraft, and supersonic aircraft
#13Trip device for enhancing performance and handling qualities of an aircraft
#14Shockwave mitigation system for supersonic aircraft
#15Rotating detonation propulsion system
#16ROTATING DETONATION ACTUATOR
#17NACELLE INTAKE
#18System and method for fluid manipulation
#19Methods and apparatus to monitor a shock wave proximate a transonic surface
#20Aircraft with strut-braced wing system
#21Aircraft portion with reduced wave drag
#22ICE DETECTION/PROTECTION AND FLOW CONTROL SYSTEM BASED ON PRINTING OF DIELECTRIC BARRIER DISCHARGE SLIDING PLASMA ACTUATORS
#23Flight vehicle with air inlet isolator having wedge on inner mold line
#24Systems and methods for generating avionic displays including forecast boom tolerance threshold exceedance symbology
#25Flight vehicle air breathing propulsion system with isolator having obstruction
#26Flight vehicle air breathing engine with isolator having bulged section
#27Shock Wave Modification Method and System
#28Shock Wave Modification Method and System
#29Aircraft wing with an adaptive shock control bump
#30System, apparatus and methods for hypersonic shockwave muffler
#31AERODYNAMICALLY ORIENTED THERMAL PROTECTION SYSTEM OF HYPERSONIC VEHICLES
#32Swept gradient boundary layer diverter
#33Shock Wave Modification Method and System
#34System and method for controlling a pressure field around an aircraft in flight
#35Superconductive Hypersonic Liquefaction Nosecone
#36Bilaterally asymmetric design for minimizing wave drag
#37Supersonic aircraft with spike for controlling and reducing sonic boom
#38System and method for minimizing wave drag through bilaterally asymmetric design
#39Shock wave modification method and system
#40Synthetic Jet Ejector With Sealed Motor
#41Shock wave modification method and system
#42Systems and Methodologies for Preventing Dust and Particle Contamination of Synthetic Jet Ejectors
#43Systems And Methodologies For Preventing Dust and Particle Contamination of Synthetic Jet Ejectors
#44Propulsion device using fluid flow
#45Shock wave modification method and system
#46Method and apparatus for controlling flow about a turret
#47Supersonic aircraft with spike for controlling and reducing sonic boom
#48Aircraft fairing
#49Shock wave modification method and system
#50Shock bump
#51Aerodynamic structure with non-uniformly spaced shock bumps
#52Aerodynamic structure with asymmetrical shock bump
#53Aerodynamic structure with series of shock bumps
#54SHOCK BUMP ARRAY
#55Flying object for transonic or supersonic velocities
#56Supersonic aircraft for reducing sonic boom effects at ground level
#57Airfoil system for cruising flight
#58Supersonic aircraft footprint spreading control system and method
#59Dynamic bumps for drag reduction at transonic-supersonic speeds
#60Active control of surface drag
#61Fuselage design for sonic boom suppression of supersonic aircraft
#62Method of controlling aerodynamic characteristics of spiked flying object, and spiked flying object
#63Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
#64Shock wave modification method and system
#65SUPERSONIC AIRCRAFT WITH SPIKE FOR CONTROLLING AND REDUCING SONIC BOOM
#66Shock wave modification method and system
#67Canard position and dihedral for boom reduction and pitch/directional control
#68Conformal aero-adaptive nozzle/aftbody
#69Methods and systems for controlling lower surface shocks
#70SUPERSONIC AIRCRAFT WITH SPIKE FOR CONTROLLING AND REDUCING SONIC BOOM
#71Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
#72Trailing vortex management via boundary layer separation control
#73Supersonic aircraft with channel relief control
#74Aircraft thickness/camber control device for low sonic boom
#75Shock wave modification method and system
#76Canard position and dihedral for boom reduction and pitch/directional control
#77Apparatus and method for reducing a sonic boom signature