MAE Graduate Seminar - NASA

<p align="LEFT"> <b><font size="5">Preparation and Preliminary Results from NASA&rsquo;s Hybrid Wing Body Acoustics Test </font></b></p> <p> <font face="Times New Roman,Times New Roman" size="4"><font face="Times New Roman,Times New Roman" size="4">Dr. Michael Doty, Assistant Branch Head for Aeroacoustics, NASA Langley Research Center, Hampton, VA </font></font></p> <p> <b><font size="4">Friday, April 25, 2014 </font></b></p> <p> <b><font size="3">ECSB 1310 </font></b></p> <p> <b><font face="Garamond,Garamond" size="3"><font face="Garamond,Garamond" size="3">11:00 am to 12:00 pm </font></font></b></p> <p> <font face="Times New Roman,Times New Roman" size="3"><font face="Times New Roman,Times New Roman" size="3">NASA&#39;s Environmentally Responsible Aviation (ERA) Project has been investigating a Hybrid Wing Body (HWB) aircraft as a possible configuration for meeting N+2 system level goals for noise, emissions, and fuel burn. A recently completed NRA led by Boeing Research and Technology resulted in a full-scale aircraft design and wind tunnel model. This model was tested acoustically in NASA Langley&#39;s 14-by 22-Foot Subsonic Tunnel during late 2012/early 2013. The preparations leading up to this large test and preliminary results will be discussed with particular emphasis on the unique Compact Jet Engine Simulator units developed and used during the test. A general discussion of NASA Langley&rsquo;s Aeroacoustics Branch will precede the HWB portion of the talk.</font></font></p>
* Seminar Mike Doty 4_25_14.pdf  (320.4 KB)

Posted By: Kareem Ahmed
Date: Wed Apr 23 00:32:34 EDT 2014