Publication Date:
2019-07-13
Description:
Flowfield rake was designed to quantify the flowfield for inlet research underneath NASA DFRC s F-15B airplane. Detailed loads and stress analysis performed using CFD and empirical methods to assure structural integrity. Calibration data were generated through wind tunnel testing of the rake. Calibration algorithm was developed to determine the local Mach and flow angularity at each probe. RAGE was flown November, 2008. Data is currently being analyzed.
Keywords:
Aerodynamics
Type:
DFRC-941
,
47th AIAA Aerospace Sciences Meeting; Jan 05, 2009 - Jan 08, 2009; Florida; United States
Format:
application/pdf