Accession Number:

ADA007433

Title:

Supersonic Laminar Boundary Layer Flow Past a Wavy Wall with Multiple Separation Regions.

Descriptive Note:

Interim rept. 1 Jan 74-1 Jan 75,

Corporate Author:

CINCINNATI UNIV OHIO DEPT OF AEROSPACE ENGINEERING

Report Date:

1975-02-01

Pagination or Media Count:

48.0

Abstract:

Laminar flow over wave shaped walls with multiple separation bubbles were studied using an implicit finite difference technique. Solutions are presented for Mach 3 and 6, Re 100 000 and 200 000, TwTo 0.45, and 0.675 and protuberance height to width ratio from 0 to 0.1. Results are compared with empirical correlations and experimental data.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE