Publication Date:
2019-06-27
Description:
Effects of varying engine inlet Reynolds number index (0.75, 0.50, 0.25, and 0.12) and temperature (289 and 244 K) on a TFE731-2 turbofan engine were evaluated. Results were classified as either compression system effects or effects on overall performance. Standard performance maps are used to present compression system performance. Overall performance parameters are presented as a function of low rotor speed corrected to engine inlet temperature.
Keywords:
AIRCRAFT PROPULSION AND POWER
Type:
NASA-TM-X-3537
,
E-8941
Format:
application/pdf