Lawrence W. Dunbar | Researchain

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Archive | 2002

Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors

Jorge Francisco Seda; Lawrence W. Dunbar; Philip Roger Gliebe; Peter N. Szucs; John Christopher Brauer; James Edward Johnson; Thomas Ory Moniz; Gregory Todd Steinmetz

Archive | 2002

Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor

Jorge Francisco Seda; Lawrence W. Dunbar; Peter N. Szucs; John Christopher Brauer; James Edward Johnson

Archive | 2002

Gas turbine with frame supporting counter rotating low pressure turbine rotors

John B. Lawrenceburg Brauer; Lawrence W. Dunbar; Philip Roger Gliebe; James Edward Johnson; Thomas Ory Moniz; Jorge Francisco Seda; Gregory Todd Steinmetz; Peter Nicholas Szucs

Archive | 2003

Counter rotating turbofan engine

Jorge Francisco Seda; Lawrence W. Dunbar; Peter Nicholas Szucs; John Christopher Brauer; James Edward Johnson

Archive | 2002

Combined cycle pulse detonation turbine engine operating method

James Edward Johnson; Lawrence W. Dunbar; Lawrence Butler

Journal of the Acoustical Society of America | 1995

Noise‐suppressed exhaust nozzles for jet engines

Eric Alan Ford; Jeremiah Paul Wolf; Lawrence W. Dunbar

Archive | 1991

Jet engine variable area turbine nozzle

Robert Joseph Orlando; Lawrence W. Dunbar

Archive | 2003

Double-inverted aircraft gas turbine engine provided with compressor with high total pressure ratio

John Christopher Brauer; Lawrence W. Dunbar; James Edward Johnson; Jorge Francisco Seda; Peter N. Szucs; ジェームズ・イー・ジョンソン; ジョルジェ・エフ・セダ; ジョン・シー・ブラウアー; ピーター・エヌ・シュッツ; ローレンス・ダブリュー・ダンバー

Archive | 1990