Aerospace
Technical Paper

INVISCID AND VISCOUS SIMULATIONS OF HIGH ANGLE OF ATTACK FLOWS

851820

11/1/1985

Event
Aerospace Technology Conference and Exposition
Authors
Dale K. Ota Rockwell International Science Center Thousand Oaks, California
Sukumar R. Chakravarthy Rockwell International Science Center Thousand Oaks, California
Joseph J. Gorski Rockwell International Science Center Thousand Oaks, California
Abstract
Content
High angle of attack flow for a NACA0012 airfoil has been computed using an Euler code and a Navier-Stokes code. These codes are based on an implicit finite-volume Total-Variation-Diminishing (TVD) formulation of the convection terms. Comparison of the two solutions shows that the Euler code does not result in a realistic separated flow solution while the Navier-Stokes code does.
Meta Tags
Topics
Wings
Affiliated or Co-Author
Rockwell International Science Center Thousand Oaks, California
Details
DOI
https://doi.org/10.4271/851820
Citation
Ota, D., Chakravarthy, S., and Gorski, J., "INVISCID AND VISCOUS SIMULATIONS OF HIGH ANGLE OF ATTACK FLOWS," Aerospace Technology Conference and Exposition, Long Beach, California, United States, October 14, 1985, https://doi.org/10.4271/851820.
Additional Details
Publisher
SAE International
Published
11/1/1985
Product Code
851820
Content Type
Technical Paper
Language
English