INVISCID AND VISCOUS SIMULATIONS OF HIGH ANGLE OF ATTACK FLOWS Rockwell International Science Center Thousand Oaks, California

Format:

Conference/Event

Author/Creator:

Ota, Dale K., author.

Conference Name:

Aerospace Technology Conference & Exposition (1985-10-14 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1985

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

851820

Access Restriction:

Restricted for use by site license