Publication Date:
2019-06-28
Description:
Ejector concepts for use with a remote augmented lift system (RALS) exhaust nozzle were studied. A number of concepts were considered and three were selected as having the greatest promise of providing the desired aircraft and exhaust gas cooling and lift enhancement. A scale model test program is recommended to explore the effects of the more important parameters on ejector performance.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-CR-167906
,
NAS 1.26:167906
,
R82AEB315
Format:
application/pdf
Permalink