Representation of Ice Geometry by Parametric Functions: Construction of Approximating NURBS Curves and Quantification of Ice Roughness--Year 1: Approx

By: Administration (Nasa), National Aeronaut

Software was developed to construct approximating NURBS curves for iced airfoil geometries. Users specify a tolerance that determines the extent to which the approximating curve follows the rough ice. The user can therefore smooth the ice geometry in a controlled manner, thereby enabling the generation of grids suitable for numerical aerodynamic simulations. Ultimately, this ability to smooth the ice geometry will permit studies of the effects of smoothing upon the aerodynamics of iced airfoils. The software was applied to several different types of iced airfoil data collected in the Icing Research Tunnel at NASA Glenn Research Center, and in all cases was found to efficiently generate suitable approximating NURBS curves. This method is an improvement over the current "control point formulation" of Smaggice (v.1.2). In this report, we present the relevant theory of approximating NURBS curves and discuss typical results of the software. Dill, Loren H. and Choo, Yung K. (Technical Monitor) Glenn Research Center NASA/CR-2004-213071, E-14547 ICE FORMATION; COMPUTER PROGRAMS; APPROXIMATION; AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; CURVES; SPLINE FUNCTIONS; NONUNIFORMITY; SURFACE ROUGHNESS; SUBROUTINES; CROSS SECTIONS

• Format: Paperback
• Language: English
• ISBN: B08FKW1XZ5
• ISBN13: 9798674148333
• Release Date: January 1
• Publisher: Independently Published
• Length: 72 Pages
• Weight: 0.42 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"