Accession Number:

ADA064803

Title:

Effect of Bluntness and Angle of Attack on Boundary Layer Transition on Cones and Biconic Configurations,

Descriptive Note:

Corporate Author:

AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1978-01-01

Pagination or Media Count:

14.0

Abstract:

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE