Accession Number:

ADA007396

Title:

Experimental Study of Pilot Losses During the Rotation of Supersonic Flow through Wide Angle in Curvilinear Channels,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Amarantova,I. I.
• Sadovskii,V. S.

Report Date:

1975-02-12

Pagination or Media Count:

23.0

Abstract:

Descriptors:

• *SUPERSONIC FLOW
• *CHANNEL FLOW
• USSR
• BOUNDARY LAYER
• TRANSLATIONS
• THREE DIMENSIONAL FLOW
• DUCT INLETS
• CASCADES(FLUID DYNAMICS)

Subject Categories:

• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE