Publication Date:
2016-06-07
Description:
Small jet aircraft engines (EPA class T1, turbojet and turbofan engines of less than 35.6 kN thrust) were evaluated with the objective of attaining emissions reduction consistent with performance constraints. Configurations employing the technological advances were screened and developed through full scale rig testing. The most promising approaches in full-scale engine testing were evaluated.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA. Lewis Res. Center Aircraft Eng. Emissions; p 149-180
Format:
application/pdf