Accession Number:

AD0613463

Title:

SEPARATED FLOW STUDIES AT HYPERSONIC SPEEDS. PART II. TWO-DIMENSIONAL WEDGE SEPARATED FLOW STUDIES,

Descriptive Note:

Corporate Author:

CORNELL AERONAUTICAL LAB INC BUFFALO N Y

Personal Author(s):

Report Date:

1964-12-01

Pagination or Media Count:

70.0

Abstract:

The paper describes an experimental study of the flow patterns and distribution of heat transfer developed in regions of adverse pressure gradient and separated flow over two-dimensional models. The investigation was directed towards obtaining information on two basic problems, the separation and the reattachment of a laminar boundary layer.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE