Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics

Authors :: Masatoshi Kodera
Takeshi Kanda
Kanenori Kato
Toshihito Saito
Kan Kobayashi
Tetsuo Hiraiwa
Source :: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Publication Year :: 2003
Publisher :: American Institute of Aeronautics and Astronautics, 2003.
Abstract: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003<br />資料番号: AC1000095000<br />レポート番号: AIAA-2003-4739

Subjects :: Engineering
business.industry
Thrust
Boundary layer suction
Combustion
Boundary layer
Flow separation
symbols.namesake
Mach number
Inviscid flow
symbols
Scramjet
Aerospace engineering
business

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