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
Personal Author(s):
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.
Descriptors:
Subject Categories:
- Fluid Mechanics