Quantitative density visualization in a transonic rotorThe flow in a two foot diameter transonic rotor has been visualized using a fluorescent gas, 2, 3 butanedione, as a tracer. The technique allows the three dimensional flow to be imaged as a set of distinct planes. Quantitative static density maps can be obtained after correcting the images for distortion and nonlinearities introduced by the illumination and imaging systems. The visualized flow is compared to data taken simultaneously by high frequency pressure transducers near the rotor entrance and exit planes.
Document ID
19750036185
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Epstein, A. H. (MIT Cambridge, Mass., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 75-24Report Number: AIAA PAPER 75-24
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 20, 1975
End Date: January 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics