Aeromechanical identification systems and methods

Acoustic resonance excited heat exchange

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Aeromechanical identification systems and methods

DE-ICING SYSTEM AND METHOD

REVERSE-FLOW CORE GAS TURBINE ENGINE WITH A PULSE DETONATION SYSTEM

Acoustic resonance excited heat exchange

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Apparatus and method for operating an oscillation blade device and a system comprising the apparatus

Pulsed deicing system

Aeromechanical identification systems and methods

Piezo actuated high speed air valve used for blade and component excitation

System and method for generating electric energy

Method and system for modulated turbine cooling

Systems and methods for generating power using a combustion source

Pulsed deicing system

System and method for flow control in turbine

Pulse energy enhanced turbine for automotive turbochargers

Reverse-flow core gas turbine engine with a pulse detonation system

Method and apparatus for variable exhaust nozzle exit area

Plasma flow control inlet particle separator system

FLOW THERMAL STRESS TURBOCHARGER TURBINE HOUSING DIVIDER WALL

Clearance control

Aircraft engine with an apparatus for pulsating expiration of gas into the exhaust nozzle

Vortex cannon with enhanced ring vortex generation

Pulse detonation combustor

Device and method for controlling vortex structures in a turbulent air jet

Control system for a land-based simple cycle hybrid engine for power generation

SYSTEM AND METHOD FOR GENERATING MODULATED PULSED FLOW

Pulse detonation/deflagration apparatus and related methods for enhancing DDT wave production

Detecting ice buildup on an aircraft engine and actuating the turbofan exit nozzle to break the ice

DETONATION COMBUSTOR TO TURBINE TRANSITION PIECE FOR HYBRID ENGINE