The aerodynamics and acoustics of the over-the-wing (OTW) Quiet, Clean, Short Haul Experimental Engine (QCSEE) were tested. A boilerplate (nonflight weight), high-throat Mach number, acoustically treated inlet and a D-shaped OTW exhaust nozzle with variable position side doors were used. Some acoustic directivity results for the type "D" nozzle and acoustic effects of variations in the nozzle side door positions are included. It was found that the results are in agreement with those previously obtained.
Comparison of NASA and contractor results from aeroacoustic tests of QCSEE OTW engine
01.04.1981
Report
Keine Angabe
Englisch
Preliminary QCSEE program test results
Tema Archiv | 1977
|Preliminary QCSEE Program Test Results
SAE Technical Papers | 1977
|QCSEE over-the-Wing Engine Acoustic Data
NTIS | 1982
|Preliminary QCSEE program - Test results
NTRS | 1977
|Preliminary QCSEE program test results
NTRS | 1977
|