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Computational Investigation of a Race Car Wing With Vortex Generators in Ground Effect
Vortex generators can be applied to control separation in flows with adverse pressure gradients, such as wings. In this paper, a study using three-dimensional steady computations for an inverted wing ...

A Method to Generate Propulsor Side Forces

J. Fluids Eng.  -- February 2010 --  Volume 132,  Issue 2, 021101 (9 pages)
doi:10.1115/1.4000745

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Author(s):
Stephen A. Huyer, Amanda Dropkin, James Dick, and David Beal
Naval Undersea Warfare Center, Code 8233, Building 1302/2, Newport, RI 02874
A computational study was performed to investigate a method to generate vehicle maneuvering forces from a propulsor alone. A ducted, preswirl propulsor was configured with an upstream stator row and downstream rotor. During normal operation, the upstream stator blades are all situated at the same pitch angle and preswirl the flow into the propulsor while generating a roll moment to counter the moment produced by the rotor. By varying the pitch angles of the stator blade about the circumference, it is possible to both generate a mean stator side force and subsequently vary the axial velocity and swirl that is ingested into the propulsor. The rotor then generates a side force in response to the inflow. Both potential flow and fully viscous 3D Reynolds averaged Navier–Stokes (RANS) computations were used to predict the stator forces, velocity field, and rotor response. Potential flow methods were used for initial examination of a wide variety of stator configurations. The most promising were then modeled using RANS. The RANS inflow was then computed and used as velocity boundary conditions during rotor blade design using potential flow methods. Blade parameters including blade number, rake, skew, and a combination of the two were varied to characterize their effects. RANS was used to then validate the final propulsor design. Computations demonstrated that total side force coefficients on the order of 0.1 and moment coefficients about the stator leading edge of 0.066 could be generated by the propulsor alone. This translates to an additional 50% control authority at 3 kn for current Navy 21[double-prime] unmanned undersea vehicles.

©2010 American Society of Mechanical Engineers

History: Received 24 October 2008; revised 25 November 2009; published 3 February 2010
doi: http://dx.doi.org/10.1115/1.4000745

KEYWORDS and PACS

Keywords
PACS
  • 89.20.Kk
    Engineering
  • 47.85.Dh
    Hydrodynamics, hydraulics, hydrostatics (applied)
  • 47.10.ad
    Navier-Stokes equations
  • 47.32.Ef
    Rotating and swirling flows
  • YEAR: 2010

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PUBLICATION DATA

Coden:
JFEGA4
ISSN:
0098-2202 (print)   1528-901X (online)
Publisher:
AIP is a member of CrossRef ASME

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