Accession Number:

ADA159714

Title:

Full Pseudospectral Solution to the Euler Equations of Motion for Airfoil Flow at Transonic Speeds.

Descriptive Note:

Memorandum rept.,

Corporate Author:

NAVAL RESEARCH LAB WASHINGTON DC

Personal Author(s):

Report Date:

1985-09-30

Pagination or Media Count:

16.0

Abstract:

The unsteady Euler equations of motion are solved for by full psuedospectral computational techniques. flows about a five percent half thick biconvex airfoil are obtained. Subcritical and supercritical cases are treated. Keywords Chebyshev Pseudospectral solutions Two dimensional Airfoils.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE