An experimental investigation of propeller wakes using a laser Doppler velocimeterThe results of experimental investigations on three single rotation propellers are summarized in this paper. Force measurements showed a definite improvement in efficiency at low advance ratios and in static operation due to use of proplets. Extensive velocity measurements were made using a LDV system. The large amounts of data gathered are presented to reveal clearly the tip vortex streaming back from the propeller. The velocities were also processed using momentum theorem to obtain the thrust and power radial distributions as well as the integrated thrust and power coefficients. The thrust coefficient compared well with force measurements and theoretical prediction from vortex lattice and Goldstein analysis. However, the power coefficient calculated from the momentum analysis was consistently lower than the theoretical or measured values. The measured velocities were also used to compute the vorticity and the trajectory of the tip vortex in the wake behind the propeller.
Document ID
19860034939
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sundar, R. M. (Embry-Riddle Aeronautical University Prescott, AZ, United States)
Sullivan, J. P. (Purdue University West Lafayette, IN, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-0080Report Number: AIAA PAPER 86-0080