Open Channel Foundation
Not Logged In |  | 
Open Channel Foundation


Quick Application Search:


PCPANEL_PNLGRF
Get this title!
¤ 
Get PCPANEL_PNLGRF


Foundation :: Aerodynamics Applications :: PCPANEL_PNLGRF

PCPANEL_PNLGRF

A Flow Solver for Single/Multi-Element Airfoils and Turbomachinery Blade Rows

Vortex

source code available SOURCE CODE AVAILABLE

PCPANEL/PNLGRF uses an integral equation solution (panel method) to solve two dimensional fluid flow problems on a personal computer. The solution method solves approximate governing equations of motions for the blade-toblade, steady-state flow problems in turbomachinery and has been used for several years in the design of turbomachinery blading.

PNLGRF is an interactive graphical interface program written specifically to allow visual analysis of the flow solutions generated by PCPANEL. It gives engineers a very rapid means of assessing a design's aerodynamic potential.

The combination of PCPANEL and PNLGRF provides designers a powerful yet cost effective tool. The run time for the flow solver is measured in minutes on PCs of modest power. As a result, the amount of man-hours required to design and analyze aerodynamic shapes is minimized.

The working fluid is assumed to be inviscid, irrotational, and a perfect gas. The integral equation solution used by PCPANEL calculates the flow around single or multi-element blade shapes that lie on a surface of revolution. It also can calculate flows through planer cascades and around isolated airfoils. The solution has demonstrated good isolated airfoil results for subsonic flows of Mach number 0.5 or less. Turbomachinery blade-to-blade flow solutions can be made for transonic flows; however, the method does lose accuracy with increasing Mach number. Turbomachinery solutions are the most accurate for flows with Mach numbers below 0.9.

PCPANEL's output includes the effects of compressibility, radius change, blade-row rotation, and variable stream sheet thickness. The compressible flow output is the most useful to the user. A summary of the solution, the integrated force coefficients, and details of the flow on the body surface are given.


PCPANEL/PNLGRF carries the NASA case number LEW-16325. It was originally released as part of the COSMIC collection.
   More software from National Technology Transfer Center


Open Channel Software runs entirely on Open Source Software. We return value to the Software community in the form of services and original software. Most of our content is currently available as source code, with the copyright owned by the original author, All Rights Reserved. Everything else is Copyright ©2000, 2001, 2002, 2003, 2004, 2005, 2006, 2007, 2008 Open Channel Software.

View our privacy statement.
Contact webmaster at openchannelsoftware dot org with questions.