Turbine blade including pin-fin array

BLOWER WITH INDENTATIONS

Airfoil having internal hybrid cooling cavities

Spray nozzle

Jet engine, flying object, and operation method of jet engine

Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system

Cooling flow for leading panel in a gas turbine engine combustor

Isentropic compression inlet for supersonic aircraft

Blade tip

Flow outlet

Gas turbine engine combustor with fluidic control of swirlers

Dual-vortical-flow hybrid rocket engine

Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system

Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles

Supersonic aircraft jet engine installation

TURBINE BLADE WITH IMPROVED TRAILING EDGE COOLING

Serpentine cooling circuit with T-shaped partitions in a turbine airfoil

Impeller

Cooling system having reduced mass pin fins for components in a gas turbine engine

Isentropic compression inlet for supersonic aircraft

Isentropic compression inlet for supersonic aircraft

Turbine blade tip with vortex generators

TURBINE AIRFOIL VANE WITH AN IMPINGEMENT INSERT HAVING A PLURALITY OF IMPINGEMENT NOZZLES

Combustor liner assembly with enhanced cooling system

Isentropic compression inlet for supersonic aircraft