Application of the ASP3D Computer Program to Unsteady Aerodynamic and Aeroelastic Analyses

By National Aeronautics and Space Administration

A new computer program has been developed called ASP3D (Advanced Small Perturbation - 3D), which solves the small perturbation potential flow equation in an advanced form including mass-consistent surface and trailing wake boundary conditions, and entropy, vorticity, and viscous effects. The purpose of the program is for unsteady aerodynamic and aeroelastic analyses, especially in the nonlinear transonic flight regime. The program exploits the simplicity of stationary Cartesian meshes with the movement or deformation of the configuration under consideration incorporated into the solution algorithm through a planar surface boundary condition. The paper presents unsteady aerodynamic and aeroelastic applications of ASP3D to assess the time dependent capability and demonstrate various features of the code. Batina, John T. Langley Research Center NASA/TM-2006-214277, L-19234 AEROELASTICITY; UNSTEADY AERODYNAMICS; COMPUTER PROGRAMS; PERTURBATION; POTENTIAL FLOW; SMALL PERTURBATION FLOW; DEFORMATION; CARTESIAN COORDINATES; SURFACE PROPERTIES

• Format: Paperback
• Language: English
• ISBN: B08FP7NGZG
• ISBN13: 9798674413271
• Release Date: January 1
• Publisher: Independently Published
• Length: 70 Pages
• Weight: 0.41 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"