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):

Report Date:

1975-02-12

Pagination or Media Count:

23.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE