Accession Number:

ADA007234

Title:

Experimental Study of Axisymmetric Boundary Layer on the Longitudinally Streamlined Cylinder,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1975-02-05

Pagination or Media Count:

36.0

Abstract:

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces

Distribution Statement:

APPROVED FOR PUBLIC RELEASE