Experimental investigation of non-uniform flow past propellers

An experimental investigation of non-uniform flow past a 1.615 foot, 3-bladed propeller was conducted in the Virginia Tech 6 foot by 6 foot Stability Wind Tunnel. The free stream velocity was 44.5 ft/sec and the propeller rpm 1400. A screen disk consisting of two circular meshes, one 15 inches in di...

Full description

Bibliographic Details
Main Author: Mallory, David A.
Other Authors: Aerospace and Ocean Engineering
Format: Others
Language:en
Published: Virginia Polytechnic Institute and State University 2020
Subjects:
Online Access:http://hdl.handle.net/10919/101447
id ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-101447
record_format oai_dc
spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-1014472021-01-15T05:35:07Z Experimental investigation of non-uniform flow past propellers Mallory, David A. Aerospace and Ocean Engineering LD5655.V855 1985.M244 Fluid dynamics Propellers -- Experiments An experimental investigation of non-uniform flow past a 1.615 foot, 3-bladed propeller was conducted in the Virginia Tech 6 foot by 6 foot Stability Wind Tunnel. The free stream velocity was 44.5 ft/sec and the propeller rpm 1400. A screen disk consisting of two circular meshes, one 15 inches in diameter and the other 5, along with a 30 degree wedge having a 7.5 inch radius, was used to create the non-uniform inflow. The screen disk was chosen to simulate a wake flow behind a slender body with an attached appendage. The propeller was operated at self-propelled mode with respect to the drag of the screen disk. Several types of measurements were completed on the propeller and the near wake. First, the propeller performance quantities were measured. The second type of measurements were the mean flow quantities, which included the mean velocities and static pressures. These were obtained by using a five hole yawhead probe. The third type of measurements were made with an x-wire probe, constant temperature anemometer and an r.m. s. meter. These allowed all the turbulence quantities, intensities and shear stresses, to be obtained. All turbulence quantities were averaged in the peripheral direction. The results of the mean and turbulent flow under the non-uniform flow condition are documented and discussed in detail. The 3-D non-uniform inflow caused the location of the maximum thrust to be shifted from . 7R, previously found for uniform inflow for the same propeller, to .88R while the location of maximum swirl was shifted inward from .6R to .5R. The turbulence quantities were sensitive to the non-uniform mean inflow and the upstream turbulence created by the screen disk, especially in the wake of the wedge region. This was generally observed in the form of higher turbulence intensities and shear stresses. This data can be used to verify and refine turbulent transport models and computational methods for flows of this type. M.S. 2020-12-15T19:11:38Z 2020-12-15T19:11:38Z 1985 Thesis Text http://hdl.handle.net/10919/101447 en OCLC# 13748620 In Copyright http://rightsstatements.org/vocab/InC/1.0/ xvii, 149 leaves application/pdf application/pdf Virginia Polytechnic Institute and State University
collection NDLTD
language en
format Others
sources NDLTD
topic LD5655.V855 1985.M244
Fluid dynamics
Propellers -- Experiments
spellingShingle LD5655.V855 1985.M244
Fluid dynamics
Propellers -- Experiments
Mallory, David A.
Experimental investigation of non-uniform flow past propellers
description An experimental investigation of non-uniform flow past a 1.615 foot, 3-bladed propeller was conducted in the Virginia Tech 6 foot by 6 foot Stability Wind Tunnel. The free stream velocity was 44.5 ft/sec and the propeller rpm 1400. A screen disk consisting of two circular meshes, one 15 inches in diameter and the other 5, along with a 30 degree wedge having a 7.5 inch radius, was used to create the non-uniform inflow. The screen disk was chosen to simulate a wake flow behind a slender body with an attached appendage. The propeller was operated at self-propelled mode with respect to the drag of the screen disk. Several types of measurements were completed on the propeller and the near wake. First, the propeller performance quantities were measured. The second type of measurements were the mean flow quantities, which included the mean velocities and static pressures. These were obtained by using a five hole yawhead probe. The third type of measurements were made with an x-wire probe, constant temperature anemometer and an r.m. s. meter. These allowed all the turbulence quantities, intensities and shear stresses, to be obtained. All turbulence quantities were averaged in the peripheral direction. The results of the mean and turbulent flow under the non-uniform flow condition are documented and discussed in detail. The 3-D non-uniform inflow caused the location of the maximum thrust to be shifted from . 7R, previously found for uniform inflow for the same propeller, to .88R while the location of maximum swirl was shifted inward from .6R to .5R. The turbulence quantities were sensitive to the non-uniform mean inflow and the upstream turbulence created by the screen disk, especially in the wake of the wedge region. This was generally observed in the form of higher turbulence intensities and shear stresses. This data can be used to verify and refine turbulent transport models and computational methods for flows of this type. === M.S.
author2 Aerospace and Ocean Engineering
author_facet Aerospace and Ocean Engineering
Mallory, David A.
author Mallory, David A.
author_sort Mallory, David A.
title Experimental investigation of non-uniform flow past propellers
title_short Experimental investigation of non-uniform flow past propellers
title_full Experimental investigation of non-uniform flow past propellers
title_fullStr Experimental investigation of non-uniform flow past propellers
title_full_unstemmed Experimental investigation of non-uniform flow past propellers
title_sort experimental investigation of non-uniform flow past propellers
publisher Virginia Polytechnic Institute and State University
publishDate 2020
url http://hdl.handle.net/10919/101447
work_keys_str_mv AT mallorydavida experimentalinvestigationofnonuniformflowpastpropellers
_version_ 1719372948122370048