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AIAA[removed]Flow Control Opportunities in Gas Turbine Engines W. K. Lord Pratt & Whitney East Hartford, CT
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Document Date: 2000-11-08 15:52:58


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File Size: 1,68 MB

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City

Denver / Hartford / /

Company

United Technologies Corporation / Pratt & Whitney / Aeronautics and Astronautics Inc. / /

Country

Switzerland / Sweden / /

Currency

USD / /

Event

Environmental Issue / /

Facility

American Institute of Aeronautics / Compressor stall / /

IndustryTerm

engine control systems / fighter applications / compact high-temperature electronics technology / engine applications / gas turbine applications / flow energy / actuator technologies / combustor exit gas temperature / mature such technologies / lowobservables device / gas turbine engines / gas turbine components / possible technologies / gas temperatures / airline / flow control technologies / gas-turbine combustor / technology looks / gas-turbine engine / gas turbine combustor / compression systems / engine systems / gas temperature / flow control technology / gas turbine aeroengines / peak gas temperature / chemical potential energy / recent and future technology innovations / gas-turbine engines / greenhouse gas / oil / flow control applications / aircraft gas turbine engine / energy / /

Organization

American Institute of Aeronautics and Astronautics / American Institute of Aeronautics / MIT / American Institute of Aeronautics and Astronautics Noise / American Institute of Aeronautics and Astronautics In / American Institute of Aeronautics and Astronautics Current / /

Person

Gregory Tillman / Time-Averaged Mass / Outflow / /

Position

Principal Research Engineer / Development Engineer / Senior Member / Senior Research Engineer / controller / /

Product

F-18A / F-22 / Advanced Tactical Fighter / Blended Wing Body / /

ProvinceOrState

Colorado / /

Technology

broadband / Flow Control / compact high-temperature electronics technology / flow control technology / actuator technologies / flow control technologies / /

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