... total pressure, P725; compressor discharge static pressure, Ps3; core engine fuel flow, WFE; fan rotor speed, N1; core rotor speed, ... The analog microphone setup was similar to the setup used by NASA Dryden during the static ground-run engine acoustic test. ... ______ a#39; a#39; a aquot; NOIa#39;lh NASA Array location Dryden Radar site / Fly-by-line 960603 *Wills, T. K., Cycle Deck Usera#39;s Manual for F1 10-GE-129 .
|Title||:||Flight and Static Exhaust Flow Properties of an F110-GE-129 Engine in an F-16XL Airplane During Acoustic Tests|
|Author||:||Jon K. Holzman|